NBS

PUBLICATIONS

A 1 1 1 0 4 0 7 7 1 D (

NBSIR 84-2951

The Testing of Laminates and

Synthetic Papers as Currency

Substrates

Walter J. Pummer, Elizabeth E. Toth-Debelius, and Francis W. Wang

U.S. DEPARTMENT OF COMMERCE

National Bureau cf Standards

Center for Materials Science

Polymers Division

Gaithersburg, MD 20899

Final Report for the Period

April 1, 1982 to April 1, 1984

Issued November 1984

Prepared for Office of Research and Technical Services

Rllr«au of Engraving and Printing

QC rtment of the Treasury

100 ington, DC 20228

. U56

34-2951

1934

c. 2

KATIONAL BUREAU OF STANDARDS

LIBRARY NBSIR 84-2951

THE TESTING OF LAMINATES AND

SYNTHETIC PAPERS AS CURRENCY

SUBSTRATES

Walter J. Pummer, Elizabeth E. Toth-Debelius, and Francis W. Wang

U.S. DEPARTMENT OF COMMERCE

National Bureau of Standards

Center for Materials Science

Polymers Division

Gaithersburg, MD 20899

Final Report for the Period

April 1, 1982 to April 1, 1984

Issued November 1984

Prepared for Office of Research and Technical Services

Bureau of Engraving and Printing

Department of the Treasury

Washington, DC 20228

U.S. DEPARTMENT OF COMMERCE, Malcolm Baldrige, Secretary

NATIONAL BUREAU OF STANDARDS, Ernest Ambler. Director

Table of Contents

Executive Summary 5

Introduction 7

Objectives for the Project 7

Part A: Laminates 8

I. Procurement of Plastic Films, Adhesives and Currency Papers .... 8

II. Paper Cutting and Accountability 10

III. Lamination Methods 11

a. Compression Molding 11

1 . Apparatus 11 2. Sample Layup 12

b. Roll Lamination 13

1 . Apparatus 13

2. Sample Layup 14

IV. Procedure for Adhesive Application 15

V. Preparation of Laminates 16

a. General Conditions 16

b. Laminates from Non-Distinctive Currency Paper (NDCP) 17

c. Laminates from Currency Paper (Reduced Thickness, CPRT) ....17

1. From biax-polypropylene (BPP) 17

2. From polycaproamide (N-6) 18

3. From low density polyethylene (LDPE) 19

d. Test Laminates from Currency Paper (CPRT) and Various Films. 19

VI. Physical Properties of Laminates Prepared from Currency Paper

(Reduced Thickness, CPRT) 23

a. Physical Test Methods 24

1. NBS Paper Flex Test 24

2. Cantilever Stiffness 25

3. Elmendorf Tear Resistance (Internal) 25

4. MIT Fold Endurance 25

5. Thickness 26

VII. Discussion of Physical Property Results from Currency Paper (CPRT)

and the Laminates 26

a. Cantilever Stiffness and Thickness 27

b. Elmendorf Tear Resistance 28

c. MIT Fold Endurance 29

VIII. Mechanical Properties of Currency Paper (CPRT) 30

a. Mechanical Test Methods 30
4

1. Apparatus and Load Elongation Curves from Tensile Tests. 30

2. Edge Tear and Energy to Edge Tear 31

IX. Discussion of Mechanical Property Results from Currency Paper

(CPRT) and the Laminates 32

a. Tensile or Breaking Strength 32

b. Elongation and Energy to Break 33

c. Initial Modulus 33

d. Edge Tear Resistance and Energy to Edge Tear 34

X. Summary of Test Results 35

XI. Physical Properties of Test Laminates Prepared from Various

Plastic Films and Currency paper (CPRT) After Flexing 36

a. Biax-polypropylene (BPP) and Poly-vinylidene Dichloride

( PVDC ) 36

b. Nylon-6 (N-6) and Polyethylene Terephthalate (PET) 36

c. Polyvinyl Chloride (PVC) 37

d. Polyvinyl Fluoride (PVF) 38

e. Co-polymer of Ethylene and Chlorotri f luoroethylene (E-CTFE).38

f. Co-polymer of Ethylene and Tetraf luoroethylene (E-TFE) 39

g. Coated Tyvek-1058 40

h. Coated Currency Paper (CPRT) .40

Part B: Synthetic Polymeric Papers 41

I. Classification 41 a. Synthetic Papers 41 b. Plastics Papers 42

II. Physical Properties of Synthetic Polymeric Papers 42

a. Tyvek-1058 43

b. Nomex-410 and -414 45

c . Texoprint 47

III. Physical Properties of Plastic Paper and Film 48

a. Melinex-377 and Melinex-442 48

IV. Mechanical Properties of Synthetic Polymeric Papers 48

a. Tyvek-1058 49

b. Nomex-4l 0-4 , -410-5 and -41 4 51 c. Texoprint 53

V. Mechanical Properties of Plastics Paper and Film 55

a. Melinex-337 and -442 55

Part C: Discussion of Test Results and Recommendations 56

I. Currency Paper (CPRT) and the Laminates 56
5

II. Synthetic Polymeric Papers, Plastics Paper and Film 59

III. Acknowledgment 62

IV. Bibliography . 62

Appendix A - Figures, 1 to 6 64

Appendix B - Tables, 1 to 10 70

Executive Summary

This report is divided into three parts. Part A is concerned with

the preparation and testing of laminates. Part B deals with the testing

of synthetic polymeric papers obtained from the Bureau of Engraving and

Printing (BEP), while Part C includes discussion of the test results,

comparisons of property data, and recommendations associated with the

laminates and synthetic papers.

The laminates were prepared from a special currency paper having

reduced thickness (CPRT) in order to compensate for the thicknesses of the

outer plastic films. Compression molding and roll lamination techniques,

employing bench-scale sized equipment, were used to prepare these

laminates from a variety of thin, transparent, plastic films. The

complete physical and mechanical test determinations are reported for CPRT

and three laminates prepared from low density polyethylene (LDPE),

polycaproamide ( N— 6 ) , and biaxially oriented polypropylene (BPP). None of

the three laminates tested have better properties in "all" categories of

concern than "does" the. currency paper now in use. Overall, the CPRT-BPP

laminate exhibited more favorable properties in more categories than did

either N-6 or LDPE laminates. Unfortunately, the low density elongation

to break values inherent in the CPRT, especially in the machine direction

(MD), are also apparent in the laminates in the MD. For this reason, due
6

to the poor performance values for CPRT, emphasis for this project shifted

from testing CPRT-based laminates to the testing of polymeric synthetic

papers as possible currency substrates.

Three synthetic papers and two polymeric film (sheet) materials

were obtained from BEP for property determinations. The synthetic papers

were: Tyvek-1058 (high density polyethylene); Nomex-MlO and -Ml

(polyarylamide ) , and Texoprint (synthetic fibers and latexes). Two types

of Melinex film -377 and -MM2 (polyethylene terephthalate ) were also

provided for testing for reasons internal to BEP. Of the synthetic papers

tested, Nomex-MlO has better overall properties, both physically and

mechanically, than any of the materials processed. The main detriments of

Nomex-MlO are its rough hand or feel, and the fact that Nomex-MlO will

absorb approximately 1 $ water for each 1055 rise in relative humidity.

Tyvek-1058 does have higher values for Elmendorf tear resistance, MIT fold

endurance, and elongation to break, but it suffers from low cantilever

stiffness (flexed) and low initial modulus. Texoprint paper also has high

cantilever stiffness values, but when flexed, considerable loss of

stiffness occurs in the direction of flex. Texoprint paper does not meet

the minimum requirements for fold endurance in either the machine or cross

direction

The single-ply synthetic paper sheet would have advantages not

inherent in a three-ply laminate. The problems of delamination and

edge-sealing would be avoided. Although most of the synthetic papers are

polymeric in structure, the texture of the synthetic surfaces is more akin

to conventional paper than to plastic films, so that blocking tendencies,

associated with glossy film surfaces, would appear to be minimal. Still,
7

abrasion, soil, ultraviolet light resistance, printability , and esthetic

qualities of the synthetic paper selected as a currency paper substitute

would have to be evaluated.

INTRODUCTION

The cost of maintaining an adequate supply of currency could be

significantly reduced by increasing the circulation lifetime. The principal factor controlling lifetime is the deterioration of the mechanical

properties, particularly flexure, of the currency substrate. It is

well-known that synthetic polymers, either as coatings or laminates, can

improve the flexure properties of paper. Also an entirely synthetic polymer substrate would be expected to result in a more durable currency. In

addition to the choice of coatings or laminates there are a large number

of synthetic polymers that may be suitable materials. Thus, the task of

identifying a suitable system for currency is formidable without further

selection criteria. We present here the final report of our joint effort

with the Bureau of Engraving and Printing to develop such selection criteria.

Objectives for this Project

1 . To locate and obtain polymeric films and adhesives suitable for

lamination with currency paper.

2. To study the conditions necessary to produce acceptable laminates by

compression molding techniques and/or roll lamination procedures.

3. To screen potential film-currency paper laminates for cantilever

stiffness, Elmendorf tear resistance, and flex-life or delamination

properties. These tests determine whether or not candidate laminates

are processed further through the complete mechanical test program.
8

4. Determine the changes in property values of the laminates or similar

polymeric papers after flexing in both the machine and cross directions. The change, if any, in property values of the flexed laminate

determines the usefulness of the laminate as a substitute currency

substrate

5. Develop property selection criteria for successful currency paper

laminates or single sheet polymeric papers.

Part A: Laminates

I . Procurement of Plastic Films, Adhesives, and Currency Papers

For this project the assumption was made that the end product

plastic laminate of currency paper would have the same physical dimensions

as currency paper now in circulation, nominally ,- 1 5.56 cm L x 6.51 cm W x

0.0114 cm T. Of these dimensions, the gauge thickness of the plastic film

was our main priority item. On this basis, a considerable effort was

expended to locate and accumulate a wide variety of thin, colorless, and

transparent plastic films. Our primary interests were in films in the

thickness range from 12.7 pm to 25.4 pm. The actual film thickness

preferred was determined by the thickness (92 pm) of the currency paper

employed in the project. Films, with thicknesses up to 38.1 pm, were also

acquired to prepare test laminates from polymers where thin films were not

available for a specific type of plastic.

A good cross-section of coated and uncoated films of different

polymeric structures was obtained from various sources (Table 1). Some

quantities of film were not as plentiful as others, but sufficient amounts

of each type were available to produce relevant test specimens. Most of

the coated films employed polyvinylidene dichloride (PVDC) as a barrier

film. PVDC was used also as an adhesive to bond the film to currency pa-
9

per in some cases. In the event of easy film delamination during testing,

we acquired, at the same time as the films, 3ome common as well as specific adhesives (Table 2) which can be applied to the uncoated counterpart

films. In general, one type of adhesive can be used for several candidate

substrates, i.e., polar adhesives for polar substrates and non polar adhesives for non polar substrates with variations therein.

Table 1 lists the films on hand, the supplier, gauge thickness in

micrometers (pm), and the coating if applicable. The films presented in

Table 1 are of the type more generally used in the packaging industry and

are more readily available in large quantities. Some specific films such

as the fluorocarbons, are also listed because of some specific property

inherent in the polymer film. Most of the films given in Table 1 will

also accept printing with inks properly formulated for the type of polymer

involved in the laminate.

On July 7, 1982, 40 sheets (65 cm L x 65 cm W x 0.014 cm T) of

non-distinctive currency paper (NDCP) and on September 1, 1982, 100 sheets

of currency paper (63 cm L x 56 cm W x 0.0092 cm T) having reduced thickness (CPRT) for laminations with plastic films were received from Mr. John

Mercer at the Bureau of Engraving and Printing (BEP). Suitable security

arrangements were made to store the papers when not in a work situation.

The unused currency papers and scraps were set aside for return to BEP

upon completion of the project.

Several types of synthetic papers and plastic films were also

obtained from the Bureau of Engraving and Printing (BEP) for physical and

mechanical property determinations.
10

Some of the more important physical and mechanical properties and

other useful data for the plastic films on hand (Table 1) were gleaned

from many sources^ 1 »2) in addition to the technical literature provided by

the manufacturer of the films. This information served as a guide to select or eliminate certain types of films whose properties did or did not

conform to those required for currency paper laminates. Initially, primary considerations were given to those films whose moduli, tensile properties, tear and fold endurances, and elongations were in a range of

values at least equal to or better than those values associated for

unprinted currency paper (3. *0 .

II. Paper Cutting and Accountability

The currency paper having reduced thickness (CPRT) obtained from

BEP was used exclusively to prepare laminates with plastic films of

appropriate thicknesses for physical and mechanical property

determinations.

Statistical considerations led to the decision to prepare thirty

(30) laminates in each series, i.e., machine (MD) and cross (CD)

directions, to be used in this project. The thirty laminates were cut and

divided as done previously for other currency papers^»6).

a. Ten (10) laminates from CPRT cut in the machine direction (MD),

which is along the short side (56 cm) of the sheet. Each sheet produces 8

(15 x 28 cm^) pieces.

b. Ten samples prepared from CPRT cut in the cross or transverse

direction (CD), which is along the long side (63 cm) of the sheet. Each

p p sheet produces 6 (15 x 30 cm ) pieces with 1 (10 x 63 cm ) piece

remaining.
c. Ten samples to be used as controls and prepared from the above

pieces in either machine or cross directions, but will not be pre-flexed

before testing. *

To date, thirty seven sheets of CPRT have been cut into machine

direction or cross direction pieces for laminate preparations. One piece

from each cut sheet has been set aside for control testing of properties

of CPRT without lamination to provide some minimum data requirements.

To help account for the currency paper on hand and used, each sheet

was assigned a number (1 to 100). As each sheet was cut, the individual

pieces were numbered sequentially, along with its directional cut, i.e'.,

1-1, 1-2, 1-3, etc. Further cuts of each individual piece would follow

-* the same pattern, i.e., piece 1-1, further cut into two pieces would give

1-1-1 and 1-1-2. By this method, it was anticipated that a complete

record can be maintained for each sheet of CPRT. As it will be shown

later, for complete testing, each laminate was cut further into eight

additional pieces of varying dimensions for specific testing applications

(Cf, Fig. 1) (5) .

III. Lamination Methods

There are two general laboratory methods available for the

preparation of test laminates on a small scale, i.e., a) compression

molding and b) roll lamination,

a. Compression Molding Techniques

1 . Apparatus

In compression molding, the materials for the laminate (film,

adhesive and paper), sometimes called "the sandwich", were assembled

outside the press between two highly polished chrome-steel plates. When

completed, the entire assembly was placed between the heated platens of
12

the press. Some pre-heat time was allowed to bring the outer cover plates

and the inner laminate materials to the working temperature used for a

particular lamination. Pressure was then applied for a given time period,

released and the laminate assembly was removed from the press and allowed

to cool inside the cover plates.

For the large size (15 x 30 cm2

) laminations, a press of 50-ton

capacity was employed which contained 38 cm2 steam-heated/water-cooled

platens with a semi-automatic positioning mode to raise or lower the

platens. The larger press facilitates ease of operation and assures that

all laminates in the same series have received similar thermal and

pressure treatments.

Initially, a small manual press, having 23 cm2 platens, was used to

prepare small laminates (13 x 13 cm2

) from 100$ cotton paper and various

plastic films as well as from non-distinctive currency paper (NDCP) to

test laminating conditions and procedures.

1 . Sample Layup for Compression Molding

During the initial layup of the laminate materials over the metal

plate some difficulty was encountered with the thin films staying flat due

to the static electricity acquired on the film surfaces. These charges

had to be neutralized with an air ionization device several times during

the assembly process. Even when electrically neutral, these thin films

(12.7 to 19.1 pm) are difficult to handle by hand without forming creases

or wrinkles in their surfaces during the layup process. The problem of

creasing can be partially avoided by placing a backing-film or release

paper between the metal plates and the outer surfaces of the laminate

films. This allows for some movement of the film in all directions

without stretching or distorting the final laminate surfaces.
13

The dimensions of the metal laminating plates were: 35 cm L

x 20 cm W x 0.32 cm T. These oversized plates are 5 cm longer and wider

than the standard laminate size ( 30 x 1 5 cm2

) needed for this project.

With these plates, the laminate materials are completely enclosed between

the plates during compression and assures that some pressure has been

equally applied to the edges of the laminates. With plates equal in size

to the laminate materials, the edges were at or near atmospheric pressure

and complete edge-sealing of the laminate was never accomplished. In the

latter case, delamination of outer plastic film always occurred when

manually flexed in MD and CD.

The type of plastic films and conditions employed to prepare the

standard size (15 x 30 cm2

) laminates are given in Tables 3 and 4.

b . Roll Laminations

1 . Apparatus

A laboratory bench top coater-laminator apparatus was used for roll

laminations of coated or uncoated films and currency paper having reduced

thickness (CPRT). The apparatus essentially contains two 10.2 cm diameter

x 38.1 cm wide rollers. The upper roller is covered with neoprene (65

shore A durometer hardness) and the lower roller is constructed of

smooth., highly polished chrome steel which can be heated when necessary.

Two 5.1 cm air cylinders with pressure regulators, a four way valve and

pressure gauge provide tjie nip pressure adjustments. The nip opening can

be controlled by microm.etric adjustments of set screws located at each end

of the roller. For coating, the apparatus contains a dip pan which rests

upon a hot plate built into an elevator for raising or lowering the pan

beneath the lower steel roller. For simultaneous two side laminations, a

second, heated, smooth steel roller replaces the upper neoprene roller in
order to provide equivalent thermal treatment on both sides of the

laminate during processing. Due to delivery time differentials between

the arrival of the coater-laminator and the second chrome-steel roller

late in the project, only single side roll laminations were performed

during this project.

2. Sample Layup for Roll Lamination

In single-side laminations, one -side of the CPRT is first coated

with adhesive; dried to tack; then covered with the desired film, and

roll laminated under specific conditions peculiar to the adhesive and

film. The reverse side is then treated in a similar fashion while

protecting the already laminated first side with silicone release paper.

There are some difficulties encountered while using the extant equipment

under these conditions. Most noticeably, reheating of the laminated first

side causes the adhesive to soften which results in additional movement of

the laminated film which leads to the formation of occasional streaks in

the surface. Ideally, with tension unwind accessories, the films and the

coated CPRT would enter the rollers at the same time eliminating the extra

precaution necessary to remove trapped air between the adhesive and film

during preparation of the "sandwich" prior to lamination. Trapped air, if

not removed or squeezed out during the process will lead to unnecessary

blistering of the laminate. Delamination of the films will occur more

readily from a blister-containing laminate during flexing.

For these small-sized laminates (15 x 30 cm2

), the use of thin

plastic films as the outer covers requires some support backing material

to hold the "sandwich" laminate in place as it enters the rollers. Silicone release paper (127 pm) and the paper blotters (584 pm) used to protect the chrome plates in compression molding serve this purpose very
15

well. The temperature, nip opening and roll speed must be adjusted to

compensate for the differences in thickness of these support materials.

Generally the nip opening between the rollers is set at one-half of the

total thickness of the material entering the rollers. Usually, the temperature is increased, and the roll speed decreased for thick samples, to

allow for adequate heat transfer to proceed from the heated rolls through

to the laminate during processing. The conditions employed to prepare

some test laminates by roll laminations from CPRT and various plastic

films are listed in Table 5.

IV. Procedure for Adhesive Application

For the preparations of laminates from uncoated, thin (25. ^ pm)

plastic films and currency paper, it was found to be easier to manually

apply the adhesive coating to the CPRT rather than to the thin films by

the brush technique. A steel straight-edge was employed to remove excess

adhesive. This method, of coating the paper rather than the plastic film

eliminates probable solvent damage to the film surfaces due to long

residence times of the solvent during the drying period. No such surface

damage was anticipated by pre-coating the paper.

In general, the CPRT sheet is clamped to a release paper on a glass

support and the coating applied by a brush. The residence time allowed is

15 seconds for solvent based adhesives, and 30 seconds for aqueous based

systems. The excess coating is then removed by the straight edge. When

j dry, the paper is turned to the reverse side and the process is

repeated. Each side of the paper is individually coated. In this method,

the amount of coating deposited per unit area depends principally upon the

concentrations of solids in the adhesive system employed. Concentrations

of material deposited upon the surface can be varied by appropriate
16

dilution technique before application. Water based adhesive systems cause

the thin currency paper (CPRT) to pucker which results in high and low

spots when the excess adhesive is removed by a straight edge. Often, when

wet, the paper snags and tears easily during removal of the excess

adhesive. No problems of this type were encountered with solvent based

adhesives. For currency paper coated by this process, the coated surfaces

varied as much as 7.6 pm (0.3 mil) per side, but many of the high and low

spots became more even during the molding process as evidenced by the

decrease in non-uniformity in thickness of the finished laminates.

The coater-laminator apparatus arrived too late near the end of the

project for machine coating of currency paper or films to be a viable

alternative to the above brush method.

The conditions used to prepare test laminates from the coated paper

and various films are given in Tables 4 and 5, along with some visual

observations and flex behavior.

V. Preparation of Laminates

a. General Conditions for Laminations

Most of the laminates containing thin plastic films and currency

paper having reduced thickness (CPRT) were prepared by compression

molding, especially those laminates used for the specific test program

(Table 3)» Other laminates used in the screening program were prepared by

both compression molding (Table 4) and roll lamination (Table 5).

The heat seal temperature range used to prepare laminates from

coated films are those recommended by the manufacturers of the films. For

adhesive coated paper and uncoated films, the data provided by the adhesive manufacturers were employed.
IT

The two pressure ranges were: 1) contact pressures, i.e., 0-0.52

MPa and 2) low pressures, 0.52-3.^ MPa. Pressures above 3. 1

* MPa would

probably distort most of these thin films needed for this project, and as

a result, high pressure laminations were not included in this study.

b. Laminates From Non-Distinctive Currency Paper (NDCP)

Non-distinctive currency paper (NDCP) was employed as an interim

substrate for laminations with plastic films until the arrival of the thin

currency paper for use in this project. Since the thickness of the paper

is 1 40 pm (5.5 mils), laminates prepared from this paper are generally too

thick. Therefore, no mechanical property determinations were planned for

these laminates. Instead, since NDCP is assumed to have the same chemical

composition as the currency paper to be used in this project, NDCP was

employed to determine laminating conditions and to provide visual property

assessments as to seals, blistering, feel and manual flex/delamination

from a variety of plastic films. In general, the laminates prepared from

NDCP are similar to those prepared from the thin currency paper (CPRT) as

reported in Table 3- Therefore, no further work was done with NDCP.

c . Laminates From Currency Paper Having Reduced Thickness (CPRT)

The sizes of all laminates prepared from the new, thinner currency

paper (CPRT) are 15 x 28 cm^ in the MD and 15 x 30 cm^ in the CD according

to the method of cutting the paper^ 5,6 ^. The laminates discussed in this

section are listed in Table 3* These laminates were used for physical and

mechanical property determinations.

1 . From Biax-Polypropylene (BPP)

The polypropylene film used for these laminations with CPRT is

biaxially (balanced) oriented (Table 1, #17) and is coated with

polyvinylidene chloride (PVDC). The film thickness is 17.8 pm. The
18

conditions used for the preparations of these laminates are listed in

Table 3 (#1). Thirty laminates were prepared for physical and mechanical

property determinations. Due to the biaxial orientation of the film,

shrinkage of the film will occur above 100 °C in both the machine (MD) and

the cross (CD) directions. Slightly more shrinkage occurs in the MD

( —5 . 5% ) than in the CD (—4.5%) . Because of the shrinkage, it is necessary

to provide a release (backing) film between the chrome plates and the

laminate to insure smooth laminate production. Without this release film,

(in this case, PET, 25.^ vra thick), the BPP films adhere slightly to the

metal plates, and shrinkage occurs in an uneven fashion leading to a

severely blistered laminate. The laminates, prepared from BPP and

currency paper having reduced thickness (CPRT) as given in Table 3 (#1),

employed the release film procedure. The seals, flex and visual

appearances of this high gloss laminate were very good. But, as it will

be discussed in a later section, there was little or no improvement in

the propagating tear resistance for this laminate even though other

physical and mechanical properties were enhanced.

2. Polycaproamide (N-6)

The polycaproamide film used for laminations with the thin currency

paper is Nylon-6 (Table 1, #13). It is used extensively as a packaging

material. The film thickness is 15.2 pm and it is also coated with PVDC

which is used as a barrier film. Like most polyamides, Nylon-6 is

hydrophilic and will absorb moisture. The moisture content varies with

the relative humidity and at 50? relative humidity and 23 °C, Nylon-6

contains from 1 .5 to 2.0? moisture. At increased levels, moisture acts a

a plasticizer for Nylon-6 which causes some loss of stiffness in the film.

This behavior is reversible.
19

In Table 3, the conditions are given for the preparation of

laminates from N-6 and CPRT as well as some visual observations of the end

product laminate. Again, the hand and feel of these laminates were good

and no flex-delamination was observed.

In addition to the sample laminates prepared above for testing,

twenty two laminates were prepared from CPRT and biax-polypropylene (BPP)

(Table 3, #2) and polycaproamide (N-6) (Table 3. #4) which were sent to

BEP for further observational and investigational purposes.

3. Low Density Polyethylene (LDPE)

The low density polyethylene film (Table 1 , #8) used for laminate

preparation with CPRT is the type used as plastic wrapping and it can be

found in most grocery stores. The thickness of the film is 12.7 pm and at

this thickness, the film lacks sufficient stiffness to be a good laminate

material. However, by the use of high temperatures and pressures, the

film was effectively used to impregnate a coating of low density polyethylene upon the CPRT. For this coated preparation, a release film of PET

was necessary between the chrome plates and the plastic-covered paper. The

LDPE coated paper easily de-laminates from PET when cooled. With no

change in thickness between the original CPRT and the LDPE coated CPRT,

the main potential of this preparation is to bind other plastic films,

such as polypropylene, with CPRT into a laminate of proper thickness. The

conditions employed to prepare the LDPE coated CPRT are listed in Table

3. (#5) along with some visual observations of the end product,

d. Preparation of Test Laminates From CPRT and Various Plastic Films

The test samples described in this section were prepared by both

compression molding (Table 4) and roll lamination (Table 5). In most

cases, uncoated films and CPRT, coated with various adhesive formulations.
20

were the laminate materials. These laminates were prepared in order to

test the effectiveness of the adhesives to seal the films to the CPRT, and

to determine the effects of the »various combinations on the physical

properties of the laminate. The final thickness of the plastic covered

laminate also bears a direct relationship to the physical and mechanical

properties of the sample. Initially, the films were selected on the basis

of high tear resistance. These films included the fluorocarbon

copolymers, E-CTFE (Table 1, #23), and E-TFE (Table 1, #22). However, for

these fluorocarbon films, the inside surfaces of the films must be

pretreated or activated, usually by in-line corona discharge' treatment,

before low temperature bonding can be achieved. The pretreated surfaces

deteriorate with time while exposed to moisture. For these films, a

special contact adhesive (Table 2, #6) was applied to the CPRT. When dry

the adhesive forms a slightly amber colored, flexible film which still

contains a small amount of tack. Due to the cohesive strength of this

adhesive, the initial alignment of the films during the layup procedure

with the coated CPRT must be done very carefully to exclude air as the

film is applied to the currency paper. Repositioning of the films after

contact has been made is virtually impossible without developing creases

and wrinkles in the laminate surfaces. These defects cannot be removed

during processing by compression molding or roll lamination and lead to

film delaminations from the CPRT. For the fluorocarbon copolymer films,

the laminates produced by roll laminations (Table 5, #2, 3, 4 and 5),

have good stability and better overall appearances than those prepared by

compression molding (Table 4, #6, 7). All have good seals and feel,

contain no blisters, and the films did not delaminate on manual flexing.
21

Several samples of* laminates were prepared from E-CTFE and CPRT

(Table 4, #6, 7) by compression molding using the same contact adhesive.

The laminates appeared to stabilize after preparation but upon standing in

the calibration room at 50t relative humidity, all of these samples

blistered badly and the films readily delaminated from the paper, mis

was not the case for the roll laminated samples (Table 5).

In Tables 4 and 5, a number of laminates are listed that were

prepared from various films and adhesive formulations in order to provide

data concerned with cantilever stiffness (CS) and Elmendorf tear

resistance (propagating) of the laminate. Some films when laminated with

CPRT have good mechanical properties, but lack the proper stiffness or

tear resistance. The type of adhesive employed in the laminate

preparation may affect the tear resistance by absorbing the energy in the

tear front and dispersing it to the surrounding regions. In this way, it

may be possible to convert cost effective films with otherwise excellent

properties but which have low tear resistance and stiffness values into

acceptable laminate materials.

Some of the films, especially BPP and N-6, have already been used

as laminate material and their property values are known (Cf, Tables 7, 8,

9, 10). For these films, the effect of employing a different adhesive

upon tear resistance and stiffness can be readily discernible providing

that the nominal thicknesses of the laminates are maintained.

The laminates prepared as test samples from various plastic films

and adhesives are listed in Tables 4 and 5. The conditions used to

prepare the laminates as well as their visual appearances are also given

in the tables.
22

The use of the polyethylene coated CPRT as a laminate substrate

with biax-polypropylene film (Table 4, #1) resulted in a laminate which

upon manual flexing caused the bond between the paper and polyethylene to

separate and delaminate. The bond formed between the outer polypropylene

and polyethylene is much stronger than that between the paper and

polyethylene. Stable laminates from biax-polypropylene (Table 4, #2) or

polyvinylidene dichloride (Table 4, #10) were prepared from CPRT when an

adhesive especially designed for polypropylene was coated onto the CPRT.

The adhesive (Table 3, #12) is a chlorinated, low molecular weight

polypropylene and when dry, a flexible, almost colorless film is formed

which requires heat activation for bonding with the films. As it will be

shown in a later section, there were no improvements in the physical

properties of these laminates and as a result, these films were eliminated

from the program.

For the polymeric films, such as polycaproamide (Table 4, #3),

polyethylene terephthalate (Table 4, #4), polyvinyl chloride (Table 4, #8)

and polyvinyl fluoride (Table 4, #9), a general purpose adhesive based

upon polyvinyl acetate-polyethylene copolymer (Table 2, #4) was used to

coat the CPRT. Two versions of the adhesive were employed for coating the

CPRT. The aqueous based emulsion (Table 2, #4) contained 55$ solids and

usually led to laminates having thicknesses greater than needed. The

other solvent-based solution (11$ solids in methyl ethyl ketone and prepared in our laboratory) was much easier to apply and yielded laminates

close to the desired thicknesses (-114 pm). It should be noted that

polyvinyl fluoride film (Table 4, #9), even though the polymer contains a

fluorine atom, can be readily sealed to CPRT by the use of this adhesive.
Also in Table 5, several examples are given for Tyvek-1058 (#6, 7,

8) and CPRT (#9, 10) in which a topical coating was applied to the sheets

and the coatings were heat sealed by roll pressure between silicone release papers. The coating is predominantly a copolymer of ethylene and

vinyl chloride which contain some acrylamide units (Table 2, #5). The amide group allows for further curing or cross-linking to achieve inherent

strength. The coating, when dry, is clear and flexible but glossy. Some

time is required for the coating to become tack free and under these conditions, initial problems with blocking may become apparent. The coating

appears to adhere well to Tyvek-1058 and CPRT and no signs of the coating

peeling from the substrates were evident. The results of the screening

tests performed on the laminates and coated papers prepared in this grouping will be discussed in a later section.

VI. Physical Properties of Laminates Prepared From Plastic Films and

Currency Paper Having Reduced Thickness (CPRT)

The object of this project is to prepare and test plastic film/CPRT

laminates for their physical and mechanical properties. The rate of

change or deterioration of these properties after the laminate has incurred some form of stress would provide data pertaining to the durability

of the laminate. The durability data obtained from these tests could be

used then to estimate or predict circulation lifetime of the laminate.

The physical properties ^

determined for each series of plastic

film-CPRT laminates, before and after flexing, both in the machine and

cross directions, were: a) cantilever stiffness (CS), b) Elmendorf tear

resistance (EL-TR) c), MIT fold endurance, and d) the average thicknesses

of the prepared laminates. A paper flex- testing machine^) was employed

to incur stress upon the laminates. A brief description of each test pro-
2M

cedure is given below. A more detailed version of the principles involved

in the test modes can be found in the literature cited. Since the

laminates, on a weight basis, contained more paper than plastic film and

adhesive, the test methods employed the standard procedures as developed

by the Technical Association of Pulp and Paper Industries (Tappi)^)

rather than those methods published by the American Society for Testing

and Materials (ASTM) for plastic films^).

a. Physical Test Methods

Prior to testing, all sheet currency paper (CPRT) was

pre-conditioned on the dry side for 16 hours before placing the samples in

the conditioning atmosphere of 23 °C and 50 % relative humidity for an

additional 16 hours in accordance with Tappi Method T M02 OS- 70 (9). After

conditioning and flexing, the sheet specimens were cut into pieces having

the proper dimensions required for a specific test program as shown in

Figure 1^). These specimens were cut from both the flexed and unflexed

(controls) samples in the machine and cross directions.

1 . NBS Paper Flex Test

Although the NBS paper flexing machine was specially designed to

promote fiber to fiber de-bonding (deterioration) in paper products in a

reproducible and uniform manner, the apparatus can also be used to incur

stress in a laminate which may result in delamination of the film or

changes in other physical and mechanical properties of the laminate.

Flexing of the samples is performed in both the machine and cross

p directions. Generally, the laminates, 15 x 30 cnr, are flexed 1000 double

flexes over 3-18 mm rollers. The laminate is clamped to the machine at

one end, while the other is constrained by a 700 g weight. With paper

alone, flexing in the machine direction produces more drastic changes in
25

properties than flexing in the cross direction^ 5 ) . These changes in

properties of the paper become evident during subsequent testing for

stiffness, tear, fold endurance, and the tensile properties. The effect

of the plastic cover on the CPRT was evaluated with respect to changes in

these properties.

2. Cantilever Stiffness Test

The Carson and Worthington Stiffness Tester C11 ) (made at NBS) was

employed to determine stiffness of the CPRT and laminates. The length and

width of the cantilever bending specimens are adjusted to enable a torque

angle reading between 30° and 120° when the sample is bent through an

angle of 25°. The test results are given in Tables 7 and 9. Again, as

the number increases, the stiffness of the paper or laminates also

increases.

3. Elmendorf Tear Test

This test is used to determine the force required to tear a single

sheet of paper or in this case, a double ply plastic laminate of paper,

after the tear has been initiated. The procedure is set forth in Tappi

Method T 4l4TS-65^). Essentially it is a measurement of the internal

tearing resistance of the paper or laminate. The larger the number, the

better tear resistance is shown by the sample. Results from these tests

are also shown in Tables 7 and 9.

4. MIT Fold Endurance Test

Three MIT fold testers were used with a 1 kg tension employing the

procedures as defined in the Standard Tappi Method T 51 1 SU-69

1

^

. Similar to the curency paper now in use, the minimum number of folds required

in either direction is 4000 double folds. In testing sample laminates, no

significant decrease in folding endurance should occur for samples f lexer:
26

1000 times. For this evaluation, as listed in Tables 7 and 9, only the

first three member laminates in each series were run to their break point.

For the remaining samples in each series, tests were terminated after 5000

double folds for specimens having a fold endurance greater than 5000 cycles .

The thicknesses of the sheets of currency paper (CPRT) and its

laminates with plastic films were determined by use of a motor-operated

dial micrometer graduated from 0 to 100 in increments of 0.0001 inches.

The thicknesses of each sheet and laminate were measured at selected

VII . Discussion of Physical Property Results of CPRT and the Laminates

The results from testing the uncovered CPRT (#2) and those of its

laminates, i.e., low density polyethylene (LDPE, #3)» polycaproamide

(N-6, #4), and biax-polypropylene (BPP, #5) for stiffness, tear, fold endurance and average thickness are given in Tables 7 and 9. In each case,

the unflexed sample, whether in machine or in cross directions, would represent the properties of the paper or laminate as prepared (controls).

The results listed for the flexed samples are those associated with some

stress or deterioration of the samples. However, to provide some basis

for comparisons, some data related to the tests here were provided by Mr.

John Mercer, BEP, for currency papers," unprinted (UCP, #1a) and printed

( PCP , # 1 b ) . The data associated with these currency papers also appear in

5. Thickness

points according to Tappi Method T 411 0S-76 (9) an(j the thickness was reported

Tables 7 and 9.
27

Paper is known to deteriorate more rapidly when flexed in the machine direction; while flexing in the cross direction produces only moderate changes in physical properties such as stiffness, tear resistance and

fold endurance. Normally, paper is stiffer in the machine direction and

more energy is required to bend the sample in the machine direction than

in the cross direction. This result is also found in our tests for currency papers as well as the laminated samples of unflexed specimens. After flexing, the differential property deterioration of these samples

again appears greater for the MD than in the CD, similar to currency paper .

a. Cantilever Stiffness and Thickness

The thickness of the sample is an important parameter of stiffness

as well as for the other properties of currency papers and the laminates.

This is readily shown when comparing the thicknesses of currency paper,

UCP (# la) and CPRT (#2). Printed currency paper (#1b) has a thickness

smaller than unprinted currency paper due to processing conditions. Considering the differences in test properties between currency papers,

UCP(#1a) and CPRT (#2), enclosing the CPRT in plastic does show improvements overall in going from CPRT (#2) through to BPP (#5). Covering currency paper (CPRT) with low density polyethylene (#3), a laminate in which

the average thickness is the same as the original CPRT, the stiffness in

the machine direction remains unchanged, while some changes were noted in

the cross direction. The laminates of CPRT and N-6 (#4) produced samples

of the appropriate thicknesses (114 um). This sample (#4) is more stiff

than the CPRT (#2) from which it was made, but less stiff, by a factor of

2.5 than the unprinted currency paper (UCP # la) of comparable thickness.

The BPP-CPRT laminates (#5) have stiffness values better than UCP (41 a', :n
28

the cross direction and almost as good in the machine direction. After

flexing, the changes in stiffness values for the three laminates, LDPE

(#3), N-6 (#4), and BPP (#5), are minimal while there are marked changes

in the cross direction for UCP(#1a).

Most PCP (#1b) now in circulation is redeemed when the paper becomes limp or when most of its stiffness is lost^3,^). The point at which

this limpness becomes apparent is about a value of 88 pN»m or below.

Therefore any laminate not having an original stiffness factor considerably in excess of this value would be useless. On this basis, the stiffness data as shown in Tables 7 and 9, indicate the LDPE (#3), at least in

its present form would be unacceptable as laminate material; BPP (#5) approaches PCP (#1b), in stiffness characteristics and N-6 (#M) appears in

the marginal category. If the laminate is too stiff, bending and flexural

properties become too cumbersome. On the other hand, sufficient stiffness

is required for machine processing (pushing and pulling) of the final

product laminate through the processing and dispensing equipment,

b. Elmendorf Tear Resistance

The property of propagating tear resistance (EL-TR) is, perhaps,

one of the more important characteristics desirable in a good laminate.

In this test, after the laminate is initially cut, whether in the MD or

CD, the laminate must be able to undo the stress caused by the propagating

front thereby stopping or delaying the tearing action at some point along

the path of tear. Of the three laminates processed through the complete

testing program, only N-6 (Tables 7 and 9, has a tear resistance comparable to UCP (#1a) or PCP (#1b). LDPE (#3) and BPP (#5) laminates do

not appear to afford additional resistance to tear once a tear has been

initiated. Both N-6 (#4) and BPP (#5) are films having a coating of
29

polyvinylidene dichloride (PVDC) in the 2-4 pm range. The difference in

EL-TR values for these two films is due to the orientation of BPP film.

This N-6 is not oriented. While biaxial (balanced) orientation does improve properties such as tensiles, etc., the EL-TR values decrease noticeably from the non-oriented PP^). Similar observations were made for

oriented N-6.

In a later section under test laminates, some laminates prepared

from films having high tear resistance qualities will be reviewed,

c. Fold Endurance of Processed Laminates

The fold endurance test (MIT) data are also presented in Tables 7

and 9 for currency papers, (UCP, #1a, PCP, #1b) and CPRT (#2) and its

laminates (LDPE) (#3), N-6 (#4), and BPP (#5). The results reported here

for CPRT (#2), LDPE (#3). N-6 (#4), and BPP (#5) are averages of the first

three samples in each series in the machine and cross directions. These

samples in each series were run till breaks occurred. All other samples

(7) in each series were run until the 5000 double fold cycles were completed. Three different MIT fold testers were used in these tests and all

results fell within the averages as listed in Table 7 and 9. The immediate concern here appears to be the wide disparity between results from UCP

(#1a) and CPRT (#2). CPRT (#2) being thinner than UCP (#1a) would be expected to have a higher fold endurance than its thicker counterpart (UCP).

But the difference observed is a factor of 5 greater in the machine direction and a factor of 3~ 3 - 5 higher in the cross direction of CPRT (#2) over

UCP (#1a). We have no ready explanation for this phenomena, unless, since

CPRT (#2) is a specially prepared paper, the composition of this paper is

not the same as UCP (#1a)
30

The fold endurance results for the laminate of LDPE (#3) and CPRT

(#2) show little or no noticeable improvement in this important property

over CPRT (#2) alone. *

Data for the N-6/CPRT (#4) and BPP/CPRT (#5) laminates indicate a

considerable enhancement in fold endurance for these laminates over both

UCP (#1a) and CPRT (#2), whether flexed or unflexed, in either machine or

cross direction modes. These results for fold endurance for N-6/CPRT (#4)

and BPP/CPRT (#5) laminates were not unexpected since N-6 or BPP alone can

survive more than 75,000 cycles without breaking.

The fold endurance data for these plastic-enclosed laminates, as

shown in Tables 7 and 9, are far superior to UCP (#1a). Most flexible

films, when available in the gauge thicknesses (13~18 pm) as required for

this project, will probably possess this desirable property. Therefore,

fold endurance of these and future laminates would not be a problem of

major concern at this time.

VIII. Mechanical Properties of CPRT and Its Laminates

a. Mechanical Test Methods

The same procedures and equipment were used to determine the

mechanical properties of CPRT and the laminates as were employed for

testing research grade currency paper as reported previously

^ »5 ,6

)

1Apparatus and Load Elongation Curves

An Instron Tensile Tester 1

, model TM-M, was used to produce

load-elongation curves from specimens 10 cm long and 1.5 cm wide while

employing a crosshead speed of 1 cm per minute. The tensile properties of

these specimens were determined according to procedures as outlined in

Tappi Method, T *184-0370(9). A typical load elongation curve for a

"'cf, Disclaimer in Table 1.
31

research grade currency paper produced by this method is given in Figure

2 (6). The data of interest for this project taken from the curves were

breaking or tensile strength, elongation to break, energy to break, and »

the initial (Young's) modulus.

For paper testing, a number of conventional terms (5) are used to

define the elastic, yield and plastic regions of the curves. The initial

modulus is calculated from the initial stiffness whi-ch is derived from the

slope of line AD in the elastic portion of the curve. The plastic modulus

can also be obtained from the slope of the line DE which is taken in a

region where the curve remains straight for a short distance. Since paper

does not show a distinct yield point, the intersection of lines AD with DE

is considered to be the load at yield and therefore, the distance OB is

the elongation to yield and FG is the region of yield. The elongation to

break is determined by the line OC and the energy to break is given by the

area under the curve OEC. The area is determined by means of an

integrator attached to the chart recorder. The breaking strength is read

directly from the chart recorder at point E on the curve. Similar load

elongation curves (fig. 3 (MD) and 4 (CD)) were obtained for CPRT and the

laminates

2. Edge Tear Resistance and Energy to Edge Tear

The edge tear resistance and energy to edge tear determinations

were also performed on the same Instron Tensile Tester according to the

Tappi Method, T 470-0S66 ^). The results were obtained from specimens

10.0 cm long and 1.5 cm wide (fig. 1), and a crosshead speed of 1 cm per

minute was used^ 2 ^. The samples were torn at an angle of 20° from

horizontal. The energy to edge tear was determined from the area under

the curve by an integrator attached to the chart recorder on the tester.
32

IX. Discussion of the Mechanical Properties of CPRT and Its Laminates

a. Tensile or Breaking Strength

The data associated with the various mechanical test programs are

presented in Table 8 for samples flexed in the MD and in Table 10 for

those laminates flexed in the CD. Comparison data is also provided for

unflexed control samples as well as for the currency papers, UCP and PCP.

These test results are designed to evaluate several questions regarding

these and future laminates from CPRT i.e., 1) How good or tough are these

laminates prepared to date and, 2) How do they compare with UCP (#1a) and

PCP (#1b)? Basically, the strength of the laminate will depend upon the

properties of the substrate paper and the role of the plastic film and adhesive is to strengthen or reinforce the good qualities and to increase or

improve marginal qualities. Since the films and adhesives are the minor

components of these laminates, their contribution to the overall increase

in mechanical properties of these laminates is more than encouraging. For

example, considering the tensile strength of CPRT alone, the laminates

N-6, (#4) and BPP (#5), yield breaking strengths as good as or better than

UCP ( # 1 a ) in both MD and CD. The fact is further illustrated as shown by

the curves in figs. 3 (MD) and 4 (CD) for unflexed control samples. After

flexing, little or no change in tensile strength is observed. The

laminates of N-6 (#4) and BPP (#5), are 20-25 pm thicker than CPRT (#2)

and the LDPE laminate (#3) and this increase in thickness is reflected in

larger breaking strengths of the former laminates. However, during some

of the breaking strength tests, occasionally, the paper broke while the

film was still intact. It is not known whether this was primarily due to

poor laminate construction or to some other defect in the laminate.
33

b. Elongation and Energy to Break

The elongation to break and energy to break are measures of the

distance the paper or laminate can be stretched before rupture occurs and

in turn, the amount of work or energy required to produce this break at

some distance. The relationship is usually in the same direction, i.e.,

small elongation to break percentages result in low energy needs to produce the break. In Tables 8 and 10, these results are listed for the currency papers, UCP (# la), PCP (#1b) and CPRT (#2) along with data for the

three laminates from CPRT. The low data values for CPRT (#2) alone, especially in the MD, indicate that this property would be difficult to improve in the final laminate. As shown in figs. 3 and 4, enclosing CPRT in

plastic covers, does cause some improvement in the elongation in the MD,

but the enhancement in elongation is best shown by the BPP (#5) laminate

in the CD. Even so, the overall performances of these CPRT laminates in

this category are unsatisfactory and they do not compare favorably for

this property with the currency papers already in use.

c. The Initial Modulus

The initial or Young's modulus data are also given in Tables 8 (MD)

and 10 (CD). As mentioned earlier, the initial modulus is derived from

the slope of the line AD as shown in fig. 2 and from similar lines drawn

in figs. 3 and 4. For unflexed samples, the initial modulus is a factor

of 2 larger in the MD than in the CD. Since stiffness is directly related

to the initial modulus as the modulus changes, the stiffness also changes,

usually in the same direction, for flexed samples ^ 3) # The slope of the

lines AD in figs. 3 and 4 for the laminate BPP (#5) and N-6 (#4) are

slightly larger than for CPRT (#2) and the LDPE laminate (#3) which

results in the stiffness also being greater. However, the cross-sectional
34

areas of these former laminates are also larger due to their increased

thickness. This factor results in the near equivalency of the moduli

among the four specimens in either MD or CD. For specimens flexed in the

MD, the decrease in the initial modulus is more severe in the MD while

samples in the CD show a slight increase in the modulus brought about by a

slight increase in stiffness and a decrease in the thickness. Flexing the

samples in the CD, produces very little change in the initial modulus.

Any change in the stiffness is simply off-set by a corresponding change in

thickness of the sample. Since the initial modulus for CPRT (#2) and the

laminates, LDPE (#3), N-6 (#4) and BPP (#5), are nearly equivalent in

either MD or CD, the contributions from the plastic films to the initial

stiffness factor of the laminates would be minimal and most or all of the

stiffness of these laminates is wholly dependent upon the CPRT itself,

d . Edge Tear Resistance and Energy to Edge Tear

Generally, edge tear resistance (ED-TR) and subsequently, energy to

edge tear values are usually much higher than those values for Elmendorf

tear resistance. In ED-TR, the paper, film or laminate is not split prior

to testing and as a result, all of the energy must be expended in causing

the tear. The results for UCP (#1a), PCP (/Alb), CPRT (/A2) and the

laminates (#3,4,5) are given in Tables 8 (MD) and 10 (CD). Again, the

data show a marked improvement in values for BPP (#5) laminate over CPRT

(#2). This result is one of the more advantageous contributions that a

plastic film can provide to a laminate. No data is available at this time

for CPRT comparison with currency papers, UCP or PCP in this category.
35

X. Summary of Test Results

The complete physical and mechanical property test determinations

are reported here for CPRT (#2) and three laminates prepared from CPRT,

namely, low density polyethylene (LDPE, #3), polycaproamide (N-6, #H) and

biaxially-oriented polypropylene (BPP, #5) and where possible, comparisons

were made between the currency papers, UCP (# la), PCP (#1b) and CPRT (#2)

and the laminates. The main effect of enclosing CPRT in a plastic film

laminate, such as BPP or N-6, is to produce a product of superior fold

endurance than any of the currency papers listed in Tables 7 and 9. None

of the laminates tested to date have better properties in "all" categories

of concern than the currency papers now in use. Overall, the CPRT-BPP

laminate (#5) exhibited more favorable properties in more categories than

did either N-6 (#*0 or LDPE (#3) when compared with the currency papers,

UCP (#1a) or PCP (#1b). However, the BPP laminate also suffers from a low

Elmendorf tear resistance. Although N-6 laminate shows Elmendorf tear

resistance values as good as the currency papers, the cantilever stiffness

and edge tear resistance values for this laminate are much lower than BPP.

The low elongation to break values inherent in the CPRT especially in the

MD are also apparent in the laminates in the MD. Although values for this

property increase almost by a factor of two for BPP in the CD, it is

doubtful whether the elongation to break in the MD can be sufficiently

upgraded to produce an acceptable laminate from CPRT using the plastic

film thickness (12.7 pm) envisioned for this project. For this reason,

due to the poor performance values for CPRT, emphasis for this project

shifted from testing CPRT-based laminates to the testing of all polymeric

synthetic papers as possible currency substrates.
36

XI . Physical Properties of Test Laminates Prepared From Various Plastic

Films and CPRT After Flexing

While awaiting the arrival of the synthetic polymeric papers for

testing, some physical property measurements were determined for the

samples prepared in Tables 4 and 5. The results of these tests are given

in Table 6, for cantilever stiffness (CS) and Elmendorf tear resistance

(EL-TR) after the specimens were flexed in either MD or CD. These samples

were tested in order to determine the effects of the film, adhesive and

thickness of the laminate upon these properties.

a . Biax-Polypropylene (BPP) and Polyvinylidene Dichloride (PVDC)

In Table 6, EL-TR data are listed for test laminates of uncoated

BPP, ( A1 ) and polyvinylidene chloride (PVDC, regular film, A7). In these

two cases, the CPRT was coated with an adhesive specially designed for

polypropylene. The adhesive is a chlorinated, low molecular weight

polypropylene (Table 2 #12) and when dry, a flexible, almost colorless

film is formed which requires heat activation for bonding. The EL-TR values for these laminates (A1 , A7) are about the same order of magnitude as

the CPRT alone or the BPP/CPRT laminate (Table 7, #5). Even though some

improvement in EL-TR is shown for the adhesively bonded test sample of

BPP, ( A1 )

,

the increase was not great enough to warrant further work with

BPP and PVDC films.

b . Nylon-6 (N-6) and 'Polyethylene Terephthalate (PET)

Biaxially oriented films having the same thickness as non-oriented

Nylon-6 (N-6) usually have average tear resistance values lower than N-6

(Compare Table 6, A, BPP #1 and PVDC, #7). However, a comparison of the

EL-TR data for laminates, biax-PET/CPRT, (Table 6, A3), and N-6 (Table 6,

A2 ) with N-6 (Table 7, #4) (these laminates have about the same thick-
37

nesses) show that the EL-TR values of the PET laminate is better in the MD

and of comparable value in the CD. Both of the former laminates were

bonded with an vinylacetate-ethylene adhesive (VAE) (Table 2, #4). Yet

for the two N-6 laminates, the adhesive bonding, though different in both

cases (VAE vs PVDC), had essentially no effect upon the EL-TR values for

the N-6 laminates. Interestingly, the laminates prepared earlier from a

coated (PVDC) PET, all delaminated during the flex testing program; an indication that additional adhesion is necessary to prepare stable laminates

from PET and CPRT. A thicker version of the PET/CPRT laminate, (Table 6,

AM), gives excellent EL-TR values, but its thickness may also increase

stiffness and decrease fold resistance to an unacceptable range,

c . Polyvinyl Chloride (PVC)

Two test laminates were made from PVC and CPRT. One sample (Table

5, A5) was prepared by compression molding while the other (Table 6, B1 )

was made by roll lamination. Both samples survived the machine flexing

test without creasing or delamination. There is a considerable difference

in thickness (43 pm) between the samples due to the adhesive applications.

This difference in thickness is reflected in the test properties for

cantilever stiffness (CS) and Elmendorf tear resistance (EL-TR) values.

Sample (B1) shows excellent EL-TR values, but would appear to be too stiff

for practical purposes of handling and folding. The values for PVC sample

(A5), somewhat thinner, are in the acceptable range when compared to currency papers, unprinted (UCP, #1a) and printed (PCP, #1b) in Table 7.

This PVC film is a high gloss variety and high gloss films are prone to

develop blocking problems. Stability problems toward UV light (sunlight)

would also be suspect without incorporation of UV inhibitors into the final film.
38

d. Polyvinyl Fluoride (PVF)

Although PVF film (A6) contains a fluorine atom on the polymer

chain, no special adhesives are required to bond the film to CPRT. After

flexing, some edge delamination occurred and the test results shown in

Table 7 (A6), were performed from samples cut from the stable interior

part of the laminate. The values for CS and EL-TR, although slightly low,

would be in the acceptable range. PVF does have good abrasion and

sunlight resistance as well.

e. Copolymer of Ethylene and Chlorotrifluoroethylene (E-CTFE)

For the copolymer, E-CTFE, the lowest film thickness available at

this time is 25. *1 urn (1.0 mil). The test measurements, listed in Table 6

(B2), are from a sample which was prepared by roll lamination but was not

flexed in either MD or CD. For all of the E-CTFE-CPRT laminates, after

flexing, the surfaces of the films became very rough and ribbed, i.e., the

film surface creased and raised slightly, perpendicular to the direction

of flex. This distortion of the film surfaces occurred whether or not the

laminates were flexed in the CD or MD. To allow for complete curing of

the adhesive, some samples were flexed at 7 and days intervals after

preparation. The flex results were identical. A single sided film - CPRT

laminate was prepared for flex testing. After seven days of aging, the

laminate was flexed. The sample was first flexed with the film side down

on the roller, then flexed again in the reverse position. No signs of

creasing or ribbing were evident on the surfaces of this single sided

laminate after this treatment. The cantilever stiffness value for the

unflexed sample does not indicate that the laminate is inherently too

stiff to cause this flex creasing. Increased stiffness of the laminate

could lead to stress cracking phenomena under flexing conditions. We have
39

also observed this type of "ribbing" or cracking of the film surfaces

during flex testing of polyester (PET) laminates. The Elmendorf tear

resistance values for this laminate (B2) are excellent and when these

values are compared with the currency paper (Table 7, #1a and #1b)

data, E-CTFE (B2) is found to be far superior in this property,

f . Copolymer of Ethylene and Tetrafluoroethylene (E-TFE)

Only limited quantities of film, E-TFE, were in stock in

thicknesses of 12.7 and 25.4 pm. The test results for cantilever

stiffness and Elmendorf tear resistance for these laminates are listed in

Table 6, (B3, 12.7 pm) and (B4, 25.4 pm). The data were obtained from

samples flexed in the MD. The thinner laminate (B3) survived the flex

test without "ribbing" and no rough spots developed on the surfaces of the

films. However, some thin lines could be seen occasionally in the

laminate after flexing, but these (lines) seem to be located on the bonded

interior side of the second film (backside). The lines do not appear to

be detrimental to the flexed film. The thicker sample (B4) shows more

creases than did the thin laminate, but certainly not as much as was

observed with E-CTFE (B2). The cantilever stiffness (CS) values for the

thin E-TFE-CPRT laminate (B3) are lower than the values anticipated for a

laminate of this thickness (152.4 pm). The test laminate (B4) has better

CS values but the laminate is simply too thick for practical purposes.

Both laminates exhibit excellent EL-TR values; in fact for sample

(B4), we were unable to tear the laminate with the existing EL-TR

equipment on hand.
g. Tyvek-1058 (Manually Coated)

Two of the coated Tyvek-1058 samples (B5) and (B6), listed in Table

6, were flexed in -the CD while the third sample (B7) was flexed in the MD.

For Tyvek-1058, the MD was assumed to be in the direction taken by the

swirls of fibers in the film and again appeared to be the short side of

the sheet. After flexing, there were no signs of the coating peeling from

Tyvek-1058. The distinquishing feature among the samples is the thickness

of the coating. All three specimens still maintained excellent EL-TR values after flexing when compared to uncoated Tyvek-1058 as listed in Tables

7 and 9, (#6). As also it can be noted in Tables 7 and 9, the cantilever

stiffness values of the uncoated Tyvek-1058 decrease markedly in the direction of the flex from those values associated with the unflexed samples. One coated sample of Tyvek-1058, Table 6, B6, appears to reverse

this trend. However, since these samples in Table 6 are only preliminary

samples, not statistical samplings as those listed in Tables 7 and 9, the

trend towards better cantilever stiffness for a coated Tyvek-1058 can only

be taken as an indication that improvements in CS values are possible,

h. Coated CPRT

The physical test results for coated CPRT after flexing are given

in Table 6, (B8) and (B9). Basically, a slight enhancement of the EL-TR

values was noted from that of the uncoated CPRT (Table 7, #2) but no

significant increases were observed in the CS data even though the

thickness of these test samples approach those of UCP (Table 7 #1).
41

Part E: Synthetic Polymeric Papers

Some synthetic polymeric papers may be better suited as alternatives for use as currency papers than are laminated materials. For laminated papers, after cutting the sheet into pieces of proper size for

currency use, three types of edge materials are left exposed to the atmosphere and surroundings, the paper, the adhesive and the plastic film. Unless some means were provided to seal those edges after cutting, routine

wear and tear, and exposure of these edges to any hostile environment

probably would cause delamination of the plastic film. With synthetic

papers after cutting, these problems are avoided because the entire

surface area is virtually identical. Since synthetic papers vary greatly

in composition and structure as well as in preparation, the defects that

are found are usually inherent in the paper itself rather than in any

edge effects.

I . Classification

In the past, synthetic papers were also called ’’plastic" paper.

In recent years, some efforts have been made to distinguish synthetic

papers from plastic papers^ 1 ^ . The classification is based loosely up

on the method of preparation and the eventual end market use of the paper,

a. Synthetic Papers

Synthetic papers are classified into categories based on: (a) extruded plastics film, (b) synthetic fibers and (c) spunbonded products. In

group (a), the extruded plastic film receives a post-extrusion treatment

of either a coating material or incorporation of inorganic additives to

make the plastic film resemble paper in appearance and texture. For group

(b), synthetic fibers can be used alone or in combination with conventional paper pulp to produce synthetic paper by the usual papei—making
42

processes. In group (c), the synthetic papers are prepared from synthetic

strands of polymer, spun into interconnected fibers and finally, bonding

of the fibers together into sheets under heat and pressure.

Synthetic papers based on the above classification are more allied

with typical paper products and therefore these papers are geared for

printing and writing paper markets of the graphics industry,

b. Plastic Papers

Plastic paper, in general, does not require any post extrusion

treatment and the product is used mainly in the packaging industry as a

substitute for various paper bags, wraps and decorative functions.

II. Physical Properties of Synthetic Papers

Polymeric sheet materials were obtained from the Bureau of

Engraving and Printing (BEP) in order to compare their physical and

mechanical properties with the currency papers, unprinted (UCP), and

printed (PCP), as well as with the laminates prepared for this project.

The following sheet materials were obtained from BEP for this purpose:

1. Tyvek-1058, 2. Nomex-410 and -Ml 4, 3. Texoprint, and 4. Melinex-377 and

-442. Based on the classification discussed in the preceding sections,

Tyvek-1058, Nomex-410 and — 4 1 4 , and Texoprint are synthetic papers. The

hand and texture of this group resemble conventional paper. Melinex-377

may be typed as a plastic paper, destined for the decorative market while

Melinex-442 is simply a clear, plastic film, not classified as either a

synthetic paper or plastic paper. Both Melinex samples were tested for

internal purposes within BEP.

In general, the synthetic papers were tested in the same fashion,

using the same equipment as discussed earlier for currency paper (reduced

thickness, CPRT) and the laminates prepared from CPRT. Again, thirty
43

samples r'rom each paper were cut from sheets in both the MD and CD as well

as the samples needed for unflexed control data also in the MD and CD.

Standard test conditions of 23 °C and 50% relative humidity were employed

for all samples. The results of the physical test programs are given

below

a . Tyvek-1 058

Tyvek is prepared from high density polyethylene by first spinning

continuous strands of interconnected fibers and bonding these fibers

together into sheets under heat and pressure

(

1 5 ) . The process produces a

paper that has a fiber-swirl pattern, is white and opaque, and has smooth

surfaces. Since Tyvek is made from a high density polyethylene base, the

chemical and physical properties of the paper would be expected to be

similar to the base polymer. Tyvek is inert to most acids, bases, and

salts. It is unaffected by water, but it will swell in some organic

solvents which may cause some problems with solvent based printing inks.

Prolonged exposure to ultraviolet (UV) light causes a decrease in property values. Tyvek maintains good flexibility at low temperature (-73 °C

but begins to shrink at 118 °C and will melt at 135 °C. It is sensitive to tension-caused width loss and deformation increases at elevated

temperatures (- 107 °C). Pressure also causes shrinkage of Tyvek.

The physical properties of Tyvek-1 058 are given in Table 7, (#6),

for those samples flexed in the MD and in Table 9, (#6), for those samples

flexed in CD. In both cases, flexed samples are again compared to the

unflexed control samples. The data for the laminates prepared earlier as

well as data for UCP (#1a), PCP ( #1 b

)

and CPRT (#2) are also presented in

Table 7 and 9, for comparison purposes with the polymeric papers.
The results from the cantilever stiffness (CS) measurements of

Tyvek-1058 indicate that before flexing, this sample is about as stiff as

the N-6 laminate (#*1), but not as stiff as UCP (#1a) or the BPP laminate

(#5). After flexing Tyvek-1058, the cantilever stiffness values decrease

markedly, well below the acceptable level, in the direction of the flex

whether MD or CD. The CS values for those samples perpendicular to the

direction of flex show some stability in the CD when flexed in the MD, but

a 30J drop in CS values occurs in MD when flexed in CD. Both unflexed

values are still above the acceptable range of 88 yN*m. When flexing

Tyvek-1058 in either direction, some samples showed crease formation

along the line of flex. At present it is not known whether these creases

are related to Tyvek's sensitivity to tension caused width loss.

The Elmendorf tear resistance data (EL-TR) are also presented in

Tables 7 and 9 (#6). Due to the fiber-like swirls in the sheet,

Tyvek-1058 is very difficult to tear in a clean fashion even when pre-cut.

The tearing action under these conditions appears to mushroom the top

layer in front of the tear making it more difficult to continue, until

finally some of the top layers simply shear off on either side of the

advancing front. The EL-TR data for Tyvek-1058 show that it is as good as

the fluorocarbon-CPRT laminates (Table 6, B2, B3, B4) in this respect.

The MIT fold endurance for Tyvek-1058 is excellent and at this

thickness (168.9 uni), it rivals some of the thinner laminates listed in

Tables 7 and 9.
45

b . Nomex-410 and -414

Nomex is an aromatic nylon or polyaryl amide type of polymer. The

sheet is formed from short polymeric fibers (floe) and fibrous binder

particles by normal papermaking processes ^ 6

)

# The sheet contains no

other fillers or binders. Calendering the paper at high temperatures and

pressures bonds the constituents together to form the sheet.

Nomex sheet is tawny colored. The surfaces are not as smooth as

those of Tyvek and the hand of Nomex is harsh. Nomex will not melt or

support combustion in normal atmospheres, and has high resistance to deformation. It is generally insoluble, compatible with various oils, and

resistant to chemical and radiative degradation. Water acts as a mild

plasticizer for Nomex paper and at 50% relative humidity, Nomex retains

4—5% of moisture depending upon the thickness of the paper.

The physical properties of Nomex sheets are listed in Table 7 (#7,

8 and 9) for specimens flexed in the MD and in Table 9 for CD samples.

The Nomex sheets tested were; 410-4 (119.9 pm), 410-5 (139.2 pm) and 41

(100.1 pm). The numbers 4 and 5 after the Nomex 410 samples simply refer

to the nominal thicknesses of each sheet before conditioning and the numbers aid in distinquishing the two sheets during discussion of their properties.

Nomex-414 (#9) is too thin and lacks sufficient stiffness before

and after flexing to be of any interest as a possible currency substrate

by itself, but it was tested as a future prospect for coating or for

adhesive laminations with other films to improve its properties.

The main difference between Nomex-410-4 (#7) and 410-5 (#8) is in

the thicknesses (- 20 pm) of the samples. The greater thickness of the

Nomex-410-5 (#8) samples is reflected in better overall physical proper-
M6

ties of the latter sheet. For unflexed samples, Nomex-H10-5 (#8) has better cantilever stiffness values than does the currency papers (UCP #1a and

PCP #1b) in either MD or CD. After flexing, Nomex-410-5 (#8) retains most

of its stiffness characteristics in each direction when flexed in MD. The

major loss of stiffness for Nomex-MlO-S occurs in the CD when flexed in

the CD. The remaining stiffness of this latter sample is still greater

and well above the required minimum values than any of the currency papers

and CPRT laminates except for the BPP laminates (Table 7, #5).

The Elmendorf tear resistance (EL-TR) values given in Tables 7,

(MD) and 9, (CD) for the three Nomex samples tested, indicate that these

samples are superior to the currency papers (#1a and #1b) and the

laminates to propagating tear resistance. For' Nomex-HlO-5 (#8), whether

unflexed or flexed in either direction, the CD fraction of sample exhibits

better EL-TR values than does Tyvek-1058 (#6). The Nomex samples show

little change in EL-TR value after flexing in either MD or CD. Surprisingly, the differential thicknesses among the three samples have a smaller

than anticipated effect on the EL-TR value in the MD of the samples.

EL-TR values more akin to the CD data were expected and the difference in

value may be due to the alignment pattern of the fibers in the MD. The

Nomex samples tear more cleanly in this test than did Tyvek-1058, but a

small amount of top layer shearing during the process was also observed.

The MIT fold endurance data provided in Tables 7 (MD) and 9 (CD),

place the three Nomex samples in the acceptable range (> 5000 double folds

in each direction) on par with currency papers, UCP (#1a) and PCP (#1b)

but well below the fold endurance for Tyvek-1058 (#6) and the laminates

(#3, 4 and 5).
47

c. Texoprint

Texoprint ^

is prepared from bleached kraft fibers which is

formed into a low density absorbent sheet. The sheet is then treated with

an elastomeric polymer latex and opacifying fillers. The dried sheet is

coated on both sides with printing fillers, notably titanium dioxide and a

flexible latex binder. In this process, the usual cellulosic fiber base

is replaced by the polymeric latex. The starches, glue and casein binders

in the coating are all replaced with synthetic resins. On this basis,

Texoprint is classified as synthetic paper rather than the conventional

cellulosic paper.

The physical properties of Texoprint synthetic paper are listed in

Tables. 7 (#10 MD) and 9, (#10 CD). Texoprint paper has the highest

cantilever stiffness value in the unflexed MD of all the samples tested to

date and ranks second in the CD behind Melinex-377 (#11). After flexing,

there is a considerable decrease in these values in the direction of flex.

The residual stiffness after flexing is still above minimum values of 88

viN »m.

Unfortunately, Texoprint paper falls well below the minimum

requirements for fold endurance (> 4000 double folds in each direction)

and it has the lowest fold endurance of any of the samples listed in

Tables 7 and 9. The Elmendorf tear resistance of Texoprint paper is

equivalent to currency paper (#1a) and the N-6 laminate (#4), but it is

somewhat low for a synthetic paper of this thickness (154 vim).
48

III. Physical Properties of Plastic Paper and Film

a. Mellnex-377 and -442

The Melinexes^ 1 8) are polyester type films based on the polymer,

polyethylene terephthalate (PET). These films are biaxially oriented and

shrinkage (up to 3 %) will occur at exposure to high temperatures (190 °C).

Melinex-377 is a white, translucent matte film with low surface gloss

destined for the decorative markets. - Melinex-442 is a transparent film of

high clarity suitable for general purpose applications.

The physical properties of the Melinex-377 (#11) and -442 (#12) are

given in Ta'bles 7 (MD) and 9 (CD), for both the unflexed and flexed

samples. Melinex-377 (#11) has excellent values for cantilever stiffness,

Elmendorf tear resistance and fold endurance. Ater flexing, these values

are retained essentially unchanged. Melinex-442 (#12) has acceptable

stiffness characteristics and excellent fold endurance but the film lacks

the required Elmendorf tear resistance (> 1000 mN) as well as the proper

thickness (- 115 um).

These films, Melinex-337 and -442, were not designed for currency

paper substrates.

IV. Mechanical Properties of Synthetic Polymeric Papers

For the determinations of the mechanical properties of the

synthetic papers, the same tensile tests and procedures were employed that

were used to obtain the mechanical properties of currency paper (CPRT) and

the laminates prepared from CPRT. Again, the standard calibration

conditions of 23 °C and 50J relative humidity were adhered to for these

tests.
49

The mechanical property data can be found in Table 8, for those

samples flexed in MD and in Table 10, for those specimens flexed in the

CD. From the data in these tables, property comparisons can be made from

among the currency papers ( #1 a and #1b), CPRT (#2), the CPRT laminates

(#3, 4, 5), the synthetic papers (#6, 7, 8, 9, 10), and the plastic films

(#11 and #12).

Load elongation curves are shown in figure 5, for the above control

samples from the synthetic papers and films cut in the MD and in figure 6,

for those unflexed control specimens cut in the CD. The curves were

reconstructed on a 50 kg full scale load basis in order to accommodate

all the curves on the same graph.

Standard sample sizes (cf., fig. 1, 10 cm x 1 .5 cm) were used for

testing the mechanical properties of the synthetic papers (#6 to 10). For

the Melinex films (#11 and #12), due to their extensive elongations,

samples having 5 cm span lengths were employed in the tensile tests. the

cross head speed of the tensile test for all samples was 1 cm/minute,

a. Tyvek-1 058

The breaking strength of Tyvek-1058 (#6), is in the acceptable

range for a currency substrate material and this property is retained

substantially unchanged after flexing in either MD or CD. Although

polyethylene is considered to be an extensible polymer, Tyvek-1058 did not

"neck down" before breaking. The break was fairly clean and little

j evidence of shear was observed.

Tyvek-1058 has the largest elongation to break (%) values of the

three types of synthetic papers as well as the currency paper and

laminates. Only the Melinexes have larger values. This property of

Tyvek-1058 does not decrease materially with flexing in either direction.
50

The unflexed sample stretches slightly more in the CD before breaking than

in the MD. When flexed in the MD, there is a small decline in elongation

values for both MD and CD samples, while CD flexing causes a slight

increase in elongation results.

The energy requirements to elongate Tyvek-1058 samples to the break

point are proportional to the elongation; the more the sample elongates,

more energy is required to produce the break whether the sample was flexed

or not in either MD or CD. Almost all of the required energy is expended

in the plastic regions of curves in fig. 5 and 6.

Unflexed Tyvek-1058 has better edge tear resistance values than for

any of the other synthetic papers listed in Tables 8 and 10. Only the

CPRT-BPP laminates (#5) and Texoprint (#10) have better edge tear resistance. When Tyvek-1058 is flexed in the MD, a 46% loss of edge tear resistance occurs only in the CD portion of the sample, while flexing the

sample in the CD, major loss of edge tear resistance occurs in both MD and

CD. The large energy to edge tear values associated with unflexed

Tyvek-1058 sample, may be due to its ability to elongate and crease before

it tears.

The initial modulus is a measurement of the resistance to

deformation a material possesses in the elastic region of the load

elongation curve as shown in fig. 2.

Tyvek-1058, similar to conventional paper as also shown in fig. 2,

does not have a definite yield point (cf., figs. 5 and 6) and little energy is required to reach the yield region in either the MD or CD as the

applied load traverses through the elastic portion of the curve. The exceptionally low initial modulus for Tyvek-1058 is due to its low initial

stiffness coupled with the large cross-sectional area associated with the
51

thickness (169 ym) of the material. The average initial stiffness for

unflexed Tyvek-1058 is: MD - 112 kg or 1097.6 N, and CD « 123 kg or

1205. 4 N. When Tyvek-1058 is flexed in the MD, the initial stiffness factor (slope of line AD - fig 5) for the MD portion of the sample is decreased further by 46$, while relatively no change was observed in the CD

segments. After flexing Tyvek-1058 in the CD, both MD and CD portions of

the samples undergo considerable change in initial stiffness; the retention of the property is again less (57?) in the direction of flex. Some

changes in the thickness values of Tyvek-1058 were also noted after flexing. Since the initial modulus is derived from the slope of line AD (fig.

2) and the thickness of the sample, changes occurring in either of these

parameters after flexing also affects the value of the initial modulus,

b. Nomex-410-4, -410-5 and -414

Data for the mechanical properties of the Nomexes, 410-4 (#7),

410-5 (#8) and -41 4 (#9) are listed in Tables 8 (MD) and 10 (CD). These

data were again obtained from load elongation curves as illustrated in

figs. 5 (MD) and 6 (CD) for unflexed control samples.

Unlike Tyvek-1058, the three Nomex samples tested are generally

stronger mechanically in the MD than in the CD. After flexing in either

the MD or CD, this result (MD > CD) still persists. The differences in

property values of the Nomexes between the MD and CD as given in Tables 8

and 10 are readily discernible after comparing the curves in figs. 5 (MD)

and 6 (CD). For unflexed samples the extrapolated yield point (cf., fig.

2) for Nomex-410-5 (#8) is approximately a factor of 2 greater for the MD

over the CD and this difference does not decrease substantially after

flexing in either directions. Essentially, the energy required to stretch

the sample through the elastic yield region is twice as great for the MD
52

as it is for the CD. Although the elongations to the break points are

good in either direction for Nomex-410-5 (#8), the energy needed to oause

the break (area under the curve) is much greater in the MD again because

of the two-fold increase in the energy requirements in the elastic portion

(line AD) of the load elongation curve. Most of the total deformation

(elastic plus plastic, line OC) occur in the plastic region of the curve.

After flexing Nomex-410-5 in the MD, there is a decrease ( 8 %) in

the breaking strength of the MD portion of the sample while no change in

value occurred in this property in the CD. The decrease in breaking

strength in the MD is also accompanied by a drop in values for elongation

to break (21 . 5 %) and the energy to break ( 28 %). The property values

retained by the Nomex-410-4 (#7) and —4 1 0—5 (#8) for these categories

after flexing in the MD or CD are still considerably higher than most of

the currency papers, laminates and synthetic papers as listed in Tables 8

and 1 0

The initial moduli of Nomex-410-4 (#7) and -410-5 (#8) are lower

than CPRT (#2) and the laminates (#3, 4, 5) in either the MD or CD but not

as poor as Tyvek-1058 (#6) when the Nomexes (#7 and #8) are compared with

printed currency paper (#1 b) in the MD and especially in the CD. The

largest decrease ( 22 %) in the modulus of these samples occurs for

Nomex-410-5 (#8) in the CD after it was flexed in the CD. The decrease in

the modulus is attributed to the decrease in the slope of the line (AD) in

the elastic region of the elongation curve (fig. 6, CD) which causes a decrease in the initial stiffness parameter (4900 to 3822 N). However, the

initial stiffness for Nomex-410-5 (#8) retained is still a factor of 5

greater than Tyvek-1058 ((#6), 686 N) under similar flexing conditions.

When flexed in the MD, Nomex-410-5 (#8) undergoes the least change (< 8 %)
53

in moduli in either direction. Although the values for the initial moduli

of unflexed Nomex-410-4 (#7) are equal to the values for Ncmex-410-5 (#8)

the moduli of the former also decrease (17%) in the direction of flex

whether MD or CD.

The data for edge tear resistance and the energy required to cause

the tear for the Nomexes are provided in Tables 8 (MD) and 9 (CD). For

unflexed samples, Nomex-410-5 (#8) has edge tear resistance values

comparable to Tyvek-1058 (#6), but much lower values than the BPP/CPRT

(#5) laminate. When the samples are flexed in the MD, Nomex-410-5 (#8)

loses from 9 $ (MD) to 15 $ (CD) of its edge tear resistance while

Nomex-410-4 (#7) shows an increase in edge tear resistance from 12? (MD)

to 42$ (CD). Only Nomex-410-5 (#8) shows any loss of edge tear resistance

(MD, 12$) after flexing the samples in CD, but Nomex-410-4 (#7) yields an

equal (8$) but smaller amount of increase in both MD and CD. The energy

requirements needed to produce the edge tear in the Nomexes also vary

accordingly as the amount of the edge tear resistance changes after

flexing as shown in Tables 8 (MD) and 10 (CD),

c . Texoprint

The mechanical properties as determined for Texoprint synthetic

paper are given in Tables 8 (MD, #10) and 10 (CD, #10). Load elongation

curves for unflexed samples of Texoprint are also shown in figs. 5 (MD)

and 6 (CD). For unflexed samples, Texoprint (#10) has average breaking

strength values in the MD but much lower values in the CD for a synthetic

paper of this thickness (- 154 ym). The values for the breaking strengths

do not change significantly after flexing in either direction.
54

As shown in fig. 5 (MD), Texoprint has the lowest elongation to

break values in the MD of any of the synthetic papers tested; ranking only

above the laminates in this property. The CD portions of the unflexed

samples have elongation to break percentages comparable to Nomex-410-4

(#7) but with much lower energy to break requirements. When Texoprint

(#10) is flexed in the MD, there is a slight increase in the elongation to

break in both MD and the CD, but the energy needed to produce the break

decreased in both directions from that of the unflexed samples. Texoprint

is the only sample tested in which this occurrence was observed.

The initial modulus for unflexed Texoprint (#10) samples is

comparable to the Nomexes and Melinexes in the MD but considerably lower

than either of these papers in the CD. Flexing Texoprint (#10) in the MD

causes a severe drop in the initial stiffness (8732 ->• 3420 N) in the MD;

and as a result, only 38? of the initial modulus is retained. The CD

portion also suffers from a decrease, but smaller, in stiffness resulting

in a 66? modulus retention value. The MD flexed Texoprint also shows the

largest changes in thicknesses (increases) of any of the samples tested.

The major change in the initial modulus of Texoprint, flexed in the CD,

occurs in the CD as only 56? of the modulus value is retained while 81? of

the MD modulus is still intact. Only a slight change in thickness of the

CD sample was observed under these conditions.

The edge tear resistance of unflexed Texoprint (#10) can be placed

in the same category as Tyvek-1058 (#6) and Nomex-410-5 (#8) for the MD

region, but Texoprint is far superior to these papers in the CD; only the

BPP/CPRT (#5) has better values for edge tear resistance but less energy

is necessary to produce the edge tear in this laminate.
55

V. Mechanical Properties of Plastic Paper and Film

a . Melinex-377 and -442

The mechanical properties of Melinex-377 (#11) and -442 (#12) are

listed in Tables 8 (MD) and 10 (CD). The data were again calculated from

the load elongation curves, as shown in figs. 5 (MD) and 6 (CD) for

unflexed control samples. As stated earlier, the Melinexes are not

classed as synthetic papers but more properly as plastic films. The differences between the two species can be readily observed by comparing the

various load elongation curves in figures 5 and 6. Unlike the synthetic

or conventional papers, the region of yield* is much smaller and a more

definite yield point can be calculated for the Melinex samples. The

"humps” in the curves slightly past the yield region are due to the

Melinex samples "necking down" as it enters the plastic region. Both

Melinex samples undergo extensive elongation (MD > CD) in either direction

requiring a large amount of energy to cause the break. When the Melinexes

(#11, 12) are flexed in the MD, no significant changes occur in the property values in either the MD or CD. However, after Melinex-337 (Table 10,

#11) is flexed in the CD, all of the CD samples experience "jaw breaks" on

the tensile tester and no data for the CD could be obtained. No problems

of this type were encountered for the MD portion of the sample. The flexing of Melinex-442 (#12) in either MD or CD causes white lines to appear

at or near the edges of the samples perpendicular to the direction of the

flex. The lines extend inward from 1 to 2 cm. Since the Melinexes are

biaxially oriented, the applied stress (flexing) may have disrupted the

orientation locally allowing some segments of the polymer to crystallize.

The lines appear to be located internally in the film as the surface was
56

still smooth to the touch. Melinex-377 (#11) is white and opaque and it

could not be determined whether similar stress lines appeared after the

samples were flexed in either direction.

Part C: Discussion of Test Results and Recommendations

I. Currency Paper (Reduced Thickness) and Its Laminates

From the beginning of this project, three assumptions were made:

(1 ) the currency paper of the laminate would be printed on both sides

before the lamination process occurred; (2) the nominal thickness of the

end product laminate would be equal to the printed currency paper (115 urn

or 4.5 mils); and (3) the property values as given in Table 7, 8, 9 and 10

for the currency papers (#1a and #1b) would be used as the minimum values

acceptable for a currency paper substitute (laminate or synthetic paper)

both before and after flexing. In this latter case, not all of the data

associated with the currency papers were available as shown by the data

gaps in the tables. However, sufficient data is available for the

currency papers in most of the critical categories to provide a basis for

comparisons.

To compensate for the thicknesses of the outer plastic film covers

and adhesives of the laminate, a special currency paper (CPRT, #2) was

used for this project that was about 30 urn (25?) thinner than the

unprinted currency paper (#1a). The printing of currency paper causes

about a 8 pm decrease in the thickness (to - 115 pm) of the printed currency paper as measured from fresh, uncirculated one dollar Federal Reserve notes obtained from a local bank. Printed currency paper undergoes
57

two compressions during printing, but the laminate would have to sustain three, i.e., printing and laminating. For this reason, plastic

films having thicknesses between 12.7 and 25. ^ um could be employed depending upon the thickness of the applied adhesive. Plastic films, when

applied below their softening points, are relatively incompressible.

The reduction ( 25% ) in the thickness of the currency paper ( # 1 a ) to

the thickness of the currency paper (#2) used for this project causes considerable changes in both the physical and mechanical property values for

CPRT (# 2) in both the MD and CD. Only the MIT fold endurance and initial

modulus show any increase in property values; all of the other categories

listed yield lower values than sample #1a. The role of the plastic outer

covers and adhesives of the laminate is to provide increased protection

and durability for currency paper by improving the overall characteristics, both physically and mechanically of the currency substrate (CPRT,

#2) sufficiently above the data values for unprinted currency paper (#1a).

Larger values are not necessarily better values, but a equitable ratio of

property values between the MD and CD with at least 90% retention of property values after flexing was sought. As shown in Tables 7 to 10, CPRT

(#2) has serious physical defects in cantilever stiffness, especially in

the CD, and Elmendorf tear resistance, and mechanically in elongation to

break and edge tear resistance. Of these properties, the exceptionally

low elongation to rupture in the MD is the most detrimental to the paper

and also the most difficult defect to overcome by lamination. The

lamination of CPRT (#2) with biaxially oriented polypropylene results in a

laminate (#5) which has better property values than does the unprinted

currency paper (#1a) with respect to fold endurance, breaking strength,

and edge tear resistance. Improvement was also noted in cantilever stiff-
58

ness with excellent retention of values after flexing in both MD and CD.

The elongation to break percentage almost doubled in the CD and these values were maintained after the samples were flexed in either direction.

The small increase in the elongation to break values in the MD and the low

Elmendorf tear resistance of this BPP-CPRT laminate (#5) would be sufficient cause to reject biax-polypropylene as a laminate material.

The N-6-CPRT laminate (#4) does exhibit good Elmendorf tear

resistance and fold endurance, but it, too, suffers from low cantilever

stiffness especially in the CD and again in the elongation to break and

edge tear resistance values.

A study of the overall property results of the lamination of currency paper (#2) with plastic films (#M, 5) indicate that the process can

produce a laminated substrate with generally better properties than the

paper stock from which it was made. Only a relatively few combinations of

plastic films and adhesives from the myriad of material available were investigated in this project. Plastic films having superior property values

may eventually emerge in the marke-t place but the ideal plastic film laminate may be a compromise among the excellent, good and average property

values of the various categories listed in the tables. The currency paper

stock, used in the lamination, would have to be strengthened in many categories especially in elongation to yield and break points. These are two

mechanical properties that cannot be compromised in a currency substrate.

Several factors, other than property values of the laminates, would

have to be considered in determining the acceptability of a laminate as a

currency substrate. These are:
59

1 . Lamination of individual printed sheets would be cost

prohibitive and the process would probably have to change over

to roll printing and lamination.

2. Some method of sealing the edges of the cut laminate substrate

is required.

3. The stacking of the plastic laminates may lead to problems in

"blocking," (i.e., the inability of the plastic surfaces of the

printed sheets to slide freely over one another) caused by a

buildup of static electricity on the plastic surfaces. An

"antistat" may be incorporated in the film itself or by a spray

application of the antistat on the surfaces of the films at

some stage. Conversely, some plastics may show excess slip

characteristics, i.e., the opposite of sticking films.

4. The effect of the hot adhesive during lamination upon the

print-stability of the printed sheet.

5. The esthetic qualities of the laminate would require evaluation

for public acceptance.

II . Synthetic Papers and Plastic Films

For the synthetic papers tested in this program, it is not known

whether the same dimensions now employed for the printed Federal Reserve

notes would be adhered to in the strictest use especially in thickness

(- 115 ym). As shown in Tables 7 and 9, there is a great variance in the

thickness among the synthetic papers and plastic films tested here. Only

the Nomex-410-4 (#7) approaches the unprinted currency paper (# la) in approximate thickness of the sheet. Most of the physical and mechanical

properties of these materials will change as the thickness is varied. A

good example of these changes that can occur within the same structural
60

compositions, can be viewed by examination of the property changes based

upon the different property values of the three Nomex samples 410-4 (#7);

410-5 (#8) and 414 (#9). The thicknesses of these three samples vary by

up to 40 pm. The thicker Nomex 410-5 (139 pm) has better physical characteristics of cantilever stiffness, Elmendorf tear resistance and acceptable MIT fold endurance. Mechanically, Nomex-410-5 (#8) has better values

for -breaking strength, elongation to break, edge tear resistance and initial modulus. The main detriment of Nomex-410-5 (#8) as a currency paper

substitute may be the fact that the Nomex papers will absorb approximately

1$ water for each 10$ rise in the relative humidity to reach a maximum

value between 8-10$ at equilibrium at 95$ relative humidity ^ 6). The rate

of water absorption is highly dependent upon the thickness and density of

the paper. The absorbed water would tend to cause the paper to swell

slightly and this swelling may produce problems in handling in unconditioned automated devices. The hand or feel of the Nomexes are also relatively harsh.

Tyvek-1058 (#6) had the largest sheet thickness of all the samples

tested in this program. Unflexed Tyvek-1058 suffers from low

cantilever stiffness values and when flexed, these values fall well below

the acceptable minimum of 88 pN*m in the direction of flex. Tyvek-1058

(#6) does have high values for Elmendorf tear resistance, MIT fold

endurance, and elongation to break. However its breaking strength especially in the MD, and the initial modulus values are lower than any of the

samples tested. On this basis, Tyvek-1058 (#6) would not be an acceptable

currency paper substitute.
61

The unflexed Texoprint (#10) samples have high cantilever stiffness

values in both MD and CD, but when flexed, considerable loss of stiffness

occurs in the direction of flex. The Elmendorf and edge tear resistances

of Texoprint paper are adequate but the low values for breaking strength

(CD), elongation to break (MD) and initial modulus (CD), would eliminate

this Texoprint paper as a currency substrate. The main rejection is due

to the fact that Texoprint paper does not meet the minimum requirements

for fold endurance in either MD or CD.

The Melinexes-377 (#10) and -M42 (#11) were not designed for

currency paper substitutes. Except for the weakness of Melinex-377 (#10)

in the CD after flexing in CD, and the low Elmendorf tear resistance of

Melinex-^mg (#12), the Melinexes, in general, have good overall physical

and mechanical properties for purposes other than currency substrate.

Again, only a few synthetic papers were investigated in this

program. The single ply synthetic paper sheet would have advantages not

inherent in a three ply laminate. The problems of delamination and

edge-sealing of the laminates would be avoided. Although most of the

synthetic papers are polymeric in structure, the texture of the synthetic

surfaces is more akin to conventional paper than to plastic films, so that

blocking tendencies would appear to be minimal. Still, abrasion, soil,

ultraviolet light resistances, printability and the esthetic qualities of

the synthetic paper sel'ected as the currency paper substitute would have

to be evaluated. The studies of these additional characteristics were not

within the purview of this project.
62

Although differences were pointed out and comparisons were made

among the currency papers, laminates, synthetic papers and plastic films,

the comparisons were made mainly on a "points of interest" basis. Valid

comparisons can only be made on materials which have at least the same

nominal thicknesses.

Acknowledgments

The authors wish to thank Mr. John Mercer, liason officer for the

Bureau of Engraving and Printing and the National Bureau of Standards, for

helpful suggestions during the course of this work. Special thanks are

also due to the marketing representatives of the firms listed in Tables 1

and 2, for generous samples of their products.

Bibliography

1. Modern Plastics Encyclopedia, Society of Plastic Engineers,

McGraw-Hill, Inc-., New York, New York, 1981 -1982 Edition, pp.

540- 544 .

2. Film, Sheets and Laminates, (desk-top data bank), The International

Plastics Selector, Inc., San Diego, CA.

3. E. L. Graminski and B. W. Forshee, "Evaluation of Currency and Stamp

Papers," National Bureau of Standards Technical Report #9597,

July 31 , 1967, pp. 5-8.

4. E. L. Graminski and E. E. Toth, "Evaluation of Currency and Stamp

Papers," National Bureau of Standards Internal Report #74-571,

September 6, 1974, pp. 11-22.

5. E. L. Graminski, B. W. Forshee, and T. J. Carter, "Evaluation of

Currency and Stamp Paper," National Bureau of Standards, Technical

Report #8637, February 15, 1965, p. 2.

6. E. L. Graminski, B. W. Forshee, and T. J. Carter, "Evaluation of

Currency and Stamp Papers," National Bureau of Standards Technical

Report #9035, January 31, 1966, p. 2.

7. Technical Association of the Pulp and Paper Industries (Tappi),

Atlanta, Georgia.

8. American Society for Testing and Materials (ASTM), Philadelphia,

Pennsylvania

9. Tappi, Looseleaf Standards #1. Testing Methods and Recommended

Procedures, 1976.
63

10. Tappi, Looseleaf Standards #2. Testing Methods and Recommended

Procedures, 1976.

11. F. T. Carson and V. Worthington, Tappi, No» 1 , 36 (1953)*

12. E. L. Graminski and E. E. Toth, "Evaluation of Currency and Stamp

Papers," National Bureau of Standards Internal Report #73— T 24

,

January 30, 1973, P* 3.

13. E. L. Graminski and E. E. Toth, "Evaluation of Currency and Stamp

Paper's," National Bureau of Standards Internal Report #75-670,

February 20, 1975, p. 8.

14. Vladimir M. Wolpert, "Synthetic Polymers and the Paper Industry,"

Chapter 2, Miller Freeman Publication, Inc., 1977, p. 53.

15. Technical Bulletin, TK-1 , "Spunbonded Products," E. I. duPont de

Nemours and Company, Inc., March, 1978. Also Reference 14, p. 109

16. Technical Bulletin, NX-16, "Properties and Performance of Nomex

Aramid Paper, Type 410," E. I. duPont de Nemours and Company, Inc.

October, 1981. Also' Reference 14, p. 106.

17. Technical Bulletin, Tex-506, "Texoprint Durable Paper,"

Kimberly-Clark Corporation. Also Reference 14, p. 112.

18. Technical Bulletin, "Melinex Polyester Films", ICI Americas, Inc.,

1982.

Appendix A

Figures 1 to 6

1.5

cm

Fig. 1. Specimen Layout for Test Samples*6 *
Load,

kN.

Per

1.5

cm.

Strip

Elongation, %

Fig. 2. Typical Load-Elongation Curve for Dry-Print Currency

Paper, Cross Direction^6)
Load,

kN.

Per

1.5

cm.

Strip

3. Load-Elongation Curves for CPRT (#2) and Its

Laminates (#3, 4, 5). Unflexed Control Samples,

Machine Direction.
Load,

kN.

Per

1.5

cm.

Strip

Fig. 4. Load-Elongation Curves for CPRT (#2) and Its

Laminates (#3, 4, 5). Unflexed Control Samples, Cross

Direction.
30

25

20

15

10

5

0

c

Melinex-377 (#11)

3070 100

Elongation, %

. 5. Load Elongation Curves for Synthetic Polymeric

Papers and Films. Unflexed Control Samples, Machine

Direction.
30

25

20

15

10

5

0

Elongation, %

6. Load Elongation Curves for Synthetic Polymeric

Papers and Films. Unflexed Control Samples, Cross

Direction.
Appendix B

Tables 1 to 10

n c0 r—j rH i—

rH o O 03 Cw r—> 03 CO O O o CO <J o

-L>

— rH

a 1—1 r—» o

CO <U CO = i73 S —

O •—* £ E 3 CO j3 o a 5 O Z) o s 0) CU

CU rH

O -

1 jC i H SZ t z CU = - JH sc

Cl. e CO CJ

L CJ co Z CJ CJ .—

c <u o 0) J cu cj

a.

O cfl sc T3

a c a C~| i—c “O 4-) T3

o. c 3 E CJ c CU

a *5 <D CJ 3 l—t 0) 3 o 3 z o a j-> a O r z O * - J * H O --H 00 L-1 S a. 0 CO 3 •a rH Q_ HH rH 3 r 3 a r-H 0- =

_3 3 3 CO o = c r-H 3 O rH

O CU o rH 3 >-

O Q J Id £3 3 < a HH < Q z s: «s Q <

CL. Q_

00 3 c CU a * E E a CJ CJ CJ CJ >> rH CO £3 Q Q a i-H

•rH o > s r i II 1 > z | 1 > 1 i > o

Ci- CJ CL CL CL CL

aoo 0

rHa0

ECOCo

COcs

CO -J3O

L.13033

O'o<

coE

lx. 0

Jj

COCO CL

co CO r— -=r CM • • z • • • c

CO

m lO

CO CM on CM e*- C0 r—

<U • • • • •» c E on on -=r r- C— C— C— c— c— CM in co *— CO zr

J£

H • O o in o in CM CM CM CM CM o in in in 0 c— m CM CM in

•H CMm C\J CM »— «— r— r— r- r— CM CM on «— CM «— r— CM

aC—

CM

—

ST + i C H o * 0 IxC 0 0 2: m 1 *r4 C^- n- 0 0 0 0 0

Q. ZX in c— c

0 a

m •J rH c0 J cfl CM CM on r— *— cn 0 in —

03 3 CO GO CO 3 2: • CJ r— CL *-> -h 00 in in 1 3 X 0 0 CL 0 r-H o •rH 1 | 1 - • cu 1 4_) X 1 1 | 3 3 f-H 3 CO > > on on 3 3 3 3 3 3 (0 3 3 3 0 0 1.

CU CU 1 i CM i 03 3 Cu

O cfl 0 0 L_ 0 0 0 n rH

N 0 E 3J o o ca CO 3 3 cfl X rH z ^H H z >u z O 0 0 0 0 L-. E in 20 cfl C0 3 CO o 3 3 3 0 0 0 O 3 C\J Id on 00 00 3 CL. s: 2: z — CL a ca CE c-* c—

2C

CJO

CUE

cfl Z 30E

>1 rHo

CLaO

CU

Id 0 CM CzJ Cx. CO CJ CJ &d Cx] 1 1 L2-, EO in = ca 0 O CL Cl. E- 10 Ql O- CL CJ Cjl H CJ

hH 1 ac c < > > Q

a Cd II II II CO CL £3 CL 13 > r> 1 1 > CJ Q CL £3 _3 -T- CL z CL Cu ca ca in £3 CL Cil Cd

O3 | £3 O 3 3 0 1 0 0 0 O E H 0 3 a a 3 >. 3

uJ 0 1 » 4 —4

H rH

H 0 0 0 rH 3 3 L 0 0 c

«u> 0 >. 4J 0 >>

O

O

a 3 0 0 3 1 | 4-> 0 a 0 a rH 3 O 0 rH 0 0 0 0 0 0 •H 0 r-H •H c 0 a rH 4-> CJ r-H >% 3 < 03 0 3 •rH 3 0 3 0 E 0 0 3 0 UU 0 a a 3 0 z 0 z z u 0 0 3 0 a z z 0 z 3 rH a z z E— 0 CJ 4-) 0 3 SC 0 rH 3 rH 3 rH 0 r-H 4-) O 0 >, >> rH rH 1 c 1 0 E 0 Q. 0 >1 0 >< 0 >. a SH a 3 3 a rH >% >* 0 0 0 O >% 3 SC O 0 3 r-H -C a a a a a >> 0 O 3 3 3 rH c 3 rH 0 Cu r-H r-H a -0 4-) a 4-> 0 0 4-3 3 a —H 0 >% 0 O O E O r-H 3 > 0 0 2 0 00 0 L 0 0 a | > > rH rH 3 CL

r-H 0 r-H 0 >. •rH >. 0 >» >%

X >* >>

X >» rH 0

c—i r-H CJ r—i r-H

a

h

a rH ~ rH

H r-H rH rH < r—• r-H C2 0 d L_ CJ

O 0 z 1 0 s O = 0 O

O z z O z OO

H z z O

O 4-> 4-> 13 CJ id CJ CL Q- CL CL CL CL CL a CL CL Id U2

CM on in M3 r^- co C"' 0 OJ on zr in vO ao O' 0 <M on

r— r— r— •— •— r— •— •— •— CVJ CM (M

<lal

materials

are

Identified

to

specify

the

experimental

procedure.

Such

identification

does

not

imply

lendatlon

or

endorsement

by

the

National

Bureau

of

Standards.
Table

2.

List

of

Adhesives,

Coatings

and

Other

Agents

Used

for

Laminations.

r-i o e • (0 CJ o CJ • c £ E £ SC >

r—

sc s o »—

i-4 CO o a; tH O CO o • £ x £ o —-H m CO £ £ £ • cj O = E E O S X X O £ o esc —

03 S e e o C OO CJ 4-> o S 03 £ JC 3 m >. a 3 JC

03 cj o 1—

rH CO c £ c CJ

tH

O CO £ o CO . - rH c £ c o CJ a. X « c a o CL o s o CO Cl X S E C £ tH E E E X X o • E — — cj E 3 £ £ X i—

n CJ £ £ GO 4-> 4-> oo o •H CO 3 £ co —4 CO at < z a Cd * CO

Cx. Cd

40I z

oo

Cl

40I X

E—

Cd

CL

X>

CL

Cd

CL >

CL E

CJ> c

CL

a £ • E- o z E~

X

CD cj Cd > CJ

— 4 X

CO > CL CL - Cd CJ £ EX E

33 CL Cd t> E 03

X 1 X «* X o X 1 A E — Cd E- Cd Cd C H

r—C

H CL Cd • CJ

X

X - X

X r4X «k

X E

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X £ a

H £ X £ X

mX £ X

Cl CL £ £ - <D > — 1 CD 03 CD r a x t- Cd X —

cj

—— jc— a. » « X < co Cd CO > Cd • X c X CO X E

Cl id cj

X

X

X

X

XX i—X

X

X c CL o

-4

4-> CJ

CO o c- in > cn CO CO

—4

— co in 1 LTi CO CM CO CM in in c—

m 04 o i in in in

X . l £ CM in CM co CM

O CM CM o c*- 04 CO CO o CM CM CM

O

a

n

N 40 r— »— /\ CM r— c- /N /\ /V < E 40

CD

X ECO rH

CD o <n X CO c 03 03

CD CO £ c c a 3 o o o 4-3 4-3

4-3 £ £ 3 X 03

CD a. tH id

4-> id o s: c CO -

CD - 1-4 CD co o i 1 03 C0 03 03 > CD 1 C CD -4 c 03 C C

i—H

C £ £ CD c £ £ 03 c 03 03 o CD £ £ CD CD 3 o 03 CO 3 — E o E 3 3

oo 3 4-> 4-3 £ rH 4-> 4-3 GO rH 4-> rH rH

r-1 CO CO o 03 CO £ o 03 o o o Z E- id 3 o E- id E-1 E03

COoX£3

CLI I I

03 X

co

co jzx£X

CO XxX rH

rH >4

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CD JZ

X

C

X 03 —•035 £ 4 -H < Q Q

Xc

CDGO 03 03 03 0) 03 «< £ £ > £ > 3 3 •tH 3 tH

X £ CJ CJ 43 CJ

X

OO tH

X £ £ H

43 i 03

X 43 03 £

03 03 c £ 4-3 c £ 03 c c C

CL > 0) c 03 03 03 03 o 03 03 £

>> -4 c CD

C E- (0 CO 03C CO 03 E- tn o X o | X 43 o 03 CO 03 X < X c C c c 03 43 C0 X X 03 43 •tH JZ E E o o £ o o £ rH c E 03 £ CO C3 o o X o •H tH 03 •tH tH 3 03 E **H o >» 3 43 tH £ < CJ c CJ CO 03 E X 03 03 s: £ £ £ CJ rH 03 £ 03 43

•tH rH rH >> 3 £ rH 03

O cfl 03 tH 03 o £ o 3 3 rH rH 3 03 43 rH o 43 03 X C0 • • • 3 £ 3 3 E E o o E £ o = JZ 3 cfl £ c rH £ Q

E- CJ

H

X

XX C/3XX i CJ E- CJ

X < X a) HH

tH £

cfl 03 + 00 r-H E c n o >> o in t

c—

O CM 03 rH •H r- m 04 C— 1 tH o o t

m o X X X o X

C0 04 04 04 t o CM 40

co c o i 1 1 1 cn on CMX

X £ £

f-4 < < O o o o CM o X

XX

X

OO

C3 •tH CM on

X lO t in

m C40 0- OO CJ CJ

a

a

Q

X

X £ m O o cn 33- •=T i i 1 1 CM O i 1 i 03 i 1 CD 03 T— in 43 lO 1 i E E Jd Jd O r- 43 X 43 03 X X f— r— E Q 1 i n 1 X X C0 cfl co CO n vo CO cfl CO C 03 03 E 03 03 >. 03 03 03 -3 _3 H H i i o o o CO CQ OQ m tH rH rH 03 03 O £ 4.3 +-> rH 43 rH rH 1 1 1 1 rH rH o O o o *— CM o E X X rH rH

CJO o O (0 o X

X

OO

OO 03 03 >. >4 >> T— T— T—n CO C0 C0XX

03 o 43

O £ £ £ £ £ £ E E rH rH rH -3"Ca o C0 cfl 03 o •o 03 •o tH tH 3 3 3 3 3 3 o o o t— r— r— 03 o o E- E < < CJ <c < < a a a a Z 2 X X X < < < < id id id

C0 •k «k z X X

CJ CJ t CM m .=r in LO O'- co 04 O r- CM on -=r n 40 f- CO 04 O r” I" *— T“ CM + *
Table

3-

Laminations 3

of

Currency

Paper

(CPRT)

With

Plastic

Films

x0)

Cx. COC

co s 3 CO C rH

cO I 21 Cl) a o2 2000 : Z r 2

03 CO O I_ C 0) 03 03 03 03

C0 4-3 c C c c

C. CO 0 Z z O z 0 z 0 z

CO •H 2 2 2 2

03 rH a. CD Cl

<£

rH

CO CO T3 TO •O -O 3 rH O r r — O z O z O z

CO CO

O

OO

O

-.4 03

a

OO

a > 00

03

03

C.3 c— C- t- r—

CO CO >— s s z r— z T— z *

E

<0 a. • • • • 03 2: >— •” •“

0- o

CL

O e o

CD H

•=r co

C-0) 4-3 0.0 QQQQQQQQQQ 030) SlOSOSrojSOSO Cl. j_ •HQ OO COa) 0. rH

0) Q. n e E 03 3 00in in 00 in in in lo to in f

C0 E co pH 03 -H C

Ch CjC o

ao co CM CM • • m m CM

szH

Q.a.

CD

CC

a.01E

co

03

4-3 COc

•HE

cfl J

Q0.

CQ I>> 03 -3 C 0 03 Q. rH 1 >. X CL

CO

O

-H C. cn cl I cO O I S- 20

CL-—

CO cO O 03 I >>T3 2 S

cO =

03C >>

03 J-> rH **H >> n ^

.c c ui *j 0) a.

03

OQ

>, o

rH 3 —

O O 0 3

CM in

COcoH

4-> COc

*rH • E

c.

a

a) 2:

03 TOCM • E

*o >>

O

0) 4-3

4-3 I_ CO

CO 03 CM c O.

•*H

O S- E i- 0 • • co a. CO C

rH -

0)

O

CO 4~> •H c 0 D • 4-3 0 CrH c 03 CO •H •rH 4-) 3

CO TO

O s 3 rH

to 03 00

C CO

03 CO 0 •rH >

J- 3 X • E 03 a. •3* E CO in O C- O 03 • • O O (1) *— <*-, CO * s

CO c 03 •rH - Ou

03 r4 to 4-3 03 Cd rH E -.4 E ca CL cO co 4-> H E rH CTJ 4-3 0

cO 03 a; 4-3 <0 03 rH -C (0

CO CL 1 0] 4-3 *H 03 E a; 03 c

rH -C CO t- £_ 03 <c £— 00 cu Q- 00

CO 33

OO 03 Ci-i
Table

4.

Preparations

of

Test

Laminates

From

CPRT

and

Various

Plastic

Films

by

Compression

Molding

Techniques. c

X o

ID •H

r-t 4-3

Cjl (0c

I—( *-H CO E

3 CO C rH

CO I S 03 Q

L.a>a.

co0.E

O

1.

«*-. id

CL

co

03

>-i o o z z

cn m

<v a) bo bO z z

03 <v

a> 03 E w n E

O o a> <u O o o

CO Z >H z z CO

o m

o t. c at 03 03 a; a» 0) CD a; 0)

(0 4-> c c c c c <n 03 C c c

s_ cn o o o o o 03 03 o o o

(Q **H z z z z z >4 z z z

03 r-1 a tn Q.

«S

rH ; 03 CO Z Z Z Z z L. £. z TO z

3 rH O O O o o •rH •»H o o o n co O O O o o cfl (0 o o o

•H 0) > CO O a a a o Du Du o a u

o

•03 0) Z

<V i. •rH b0 3 C^- m in in o b- c— o o rH

ni n (8 r— CO r- on VO «

T— VO r— vO o

c. n a. • 03 a> <v s: > t. r— tr— r“

.a

cn

cn

a>u

a.

• vO CM CO CO ao vO lO vO lO co 03 a. o -=T on *=r =r -=r on • > E o r— r— t— 1— T— r— r— T— <

cn **H C3 z cn b- **H 03 • rH z cn 0 z z

cn <0 tH c rH o u*. O

t. •H t— Cd cn

03 O r— <

Q. O Q a Q Q Q o Q Q Cl a > w».

CO <u O o z: O 2: O O 2: 0 •• in

a. sl 03 in

•H > 03 Q •*H C •» cn 03 03

03 rH > z >» •*H • z z cn 03 E • CO 4-5 03 > 3 <n 03 z •H

03 CL 1 z cn

03 4-> CL 03 CO 03 E 03 3 4-3 z

rH a> ao 03 CM CM C— et •=T c— b- c z CO id z H-» c • •rH 03 4-5 < CO Du C* c— b- in in CM in m in CM CM E 4-5 03 >

o r— r— <— t— CM CM CM r— r

• <0 O E

H-H CM O c 03 cn <0 z b0 E • • •H 1 3 rH H •• O 03 s- • rH O 1 a) CM 4-5 0 0 03 0

rv -*H O •» 3 • rH Q c 3 £- a. E- /—

s

on 03 c Cd z > •rH cr 3

CL Id 03 Cil E •«H CL 0 CL > co a Z CQ CL 1 C Cu X •*H E

/-N ' >W 0 03 E- z bO 4-> z z z Z z z

CL 30 SL rH O r\ 03 in O 4-3 4-5 4-> 4D 4-3 4-5 Cl e •* 03 O >> 1 0 Du c t— 4-5 • •H •H fH •rH •«H •rH CD a> 4-> rH z CjJ-'H > > 03 <0 r— 5 3 3 3 3 3

r-s c <0 z 4-3 CL CL T3 Q3 03

1 i vO <13 -HZ 0 <13 Czl N—<r •H 4-3 z •* z Z Z Z Z z

t—' CO >. 03 o 1 rH <0 • 1 O t- Cu rH rH -H 03 m 1 03 03 03 03 03 03 03 as 03 rH C s- z >> z<~ 03 C. 03 E- >1 03 >> 03 >- 03 c 03 E 4-3 4-5 4-5 4-> 4-5 4-5 CL 0) o 03 a z 4-3 r*-X C O E CJ) C T3 c •O c -O •H s_ •rH cfl CO CTJ cfl CO CO o 4-5 CX r-H C0 4-5 z E— 03 3 >, 1 •H -*H *»H fH •rH •rH E a 4J 0 O 0 0 O O

i CO i >. O <13 03 a to rH rH rH U > s. > c. > SL <0 0 C3 0 C3 O O

E c X Q. >> -a >> 03 Cl >. <H 0 'wT >> 0 Sh 0 >> O rH 03 co rH **H co O rH •H r-H C. ’•w' Z hH Q. rH rH rH 3 rH rH 4-3 cn E- E— E H t- E-

•rH E •H L. E o E o 03 4H L O £ 0 z 0 rH 0 z rH m 03 as as rH as as as Du 03 CD Qu CL cO CL 4-> w 4L> O CL O CL Du CL 0 rH rH C- CL CL •H CL CL CL -3 < a. CL 0 0 Du 0 0 0

c\jon rr in b~ co on o * »- «xiot)(1)^6Dx:h
Table

5.

Preparations

of

Test

Samples

by

Roll

Laminations

X

Q) 4-> <-h ro

Cju

C

«H E

03 03 3 »—c C I 03 0) 2: C3

a; co o SL. 03 03 <13 d) 03 03 03 a? d) d3 c CD c c c c c c c c c C

03 .H o o o o o o o o o o

c_ CO z z z z z z z 2: z z

03 * 03 r-t CL CO CL <

rH

a z •a •a •a z Z a z -o

CT3 <0 o o o o o o o o o o 3 rH o o o o o o o o o o

CO 03

a

aa

a

a o o o aa

S_ a. co

•H

03 CL CEO •-4 03 o E E03 J Co

•H

s_ -J

d3 o

CL 03

03 S_ O- QE

ZL

CO

CO E 0)

<-t c

•-* z o a oz o o

03

C

03 Z -> CM CM CM

n

03 d3 E in in in o

V-. d> \ *— i

*

on

0. Q. E 3 00 O

00

toc

•Hc oo OO co CO

d3 1

in inn

Q. E o o o o O O • • • • o o o o

Cl

•r^ Z

d3

t- CO in in in

rH 3 03 =T in in

n rH CO 03 • • • • O co a. o o o o K 03 S mOQ

ST

in

CM o o

onm

Q

2:

QQ

O S

in

CM

-3" tLTi CM

CM r- o o o o o o z z z z z z n n n n CM CM o o o o n n rommoir- »—

CO CO CO CO CO CO o o o o o o o o o o o o

ip in in in cn iri in in in in in in o o o o o o o 3- 3 3 CO CO on «— — O o Q Q Q Q Q Q s o o s: s: s

<u d) d> d) <u 1 in ino o in

in -=r CM r- co o on — cm —

co z

d)co

4J

CD zJ

d) z

03E

Cd

<C

d)c

d) I—<

>> z

4-5 d)Id>

4-5 03

4-> d)o

03

r-4 >1c

CO > 03 z o -a O 03

a

dj zc

d>

C-3

4-5 03

5-03aE

d>

j->

4-5 03 z

d> iH

03

03

COO

i- • CO to c C ~t

-H 4-5

4-> 03

03O

OO

O

a

— 03

co **h •O rH

”“H Q.

r-H Q. O 03

•rH 03

C E Cu-, Z S- o CTJ V*. o

fc-» 3 •rH rH

n CO 4J i n 03

to 3 o z

03

H l_ • •rH 0. 03 c_ o 3 o (0

03 CL <0 o o \ 1 E Cd in 0) .Q o >> Cx* 03 z z CO '—

0. rH 03 d> E- 4-> 4-> 4-J | 03 <J o o £_ C 1 03 •rH •rH Cjl c > rH CL 4-> 03 Cd 03 3 3 < nc

CL. sz o O 03 rH >—r o •rH 03

03 1 C-3 /^S >, CO •o -a Z z rH

6- CO pH 1 o a Id i z C- o n c 03 03 4-> Z cr 03 >, 03 03 SC. 03 — CX4 03 4H 03 o •rH 4_> 4-> a. ±-> C 03 C O C Cd E- C 03 S Cd r— 03 03 3 o 03 •rH *fH 03 3 03 Cz. O 03 O >» CX4 i «0 O O 03 i C > 0. rH rH I-H H 1 rH t_ rH E—< = = T3 c_ 0) 03 o to E **H :n o >. 4-i >. o Cd >, o O Cd 03 e- 03 03 03 <H S rH rH Z —1 Z 1 ' ' z 3 CL > cr Z E- E- 4-) 0.

•rH 03 o z 4J 0- 4-5 Cd 4-) «H

O >> Q- E cr cr 03 0)

Cjh j Ou CJ Cd

H 03

w z Cd 4_ CJ = E— CJ 3 CL a. o > Z o CJ <J <c CM m n 03 t- CO O' o•— 0) o 03 z 03
Table

6.

Some

Physical

Properties

of

Test

Laminates

Prepared

From

CPRT

and

Various

Plastic

Films

After

Flexing.

Elmendorf

Cantilever

Stiffness

Tear

Resistance

Thickness

Flex

•o

0)x

<u r—

l

c

=> co

X

XX X X XX

Q X X X X

s

X X X XX

• oo in -=r on o CM =T C- CM o on O' in CM n • • • • • • • • • fH -=X -=X in ms •3" -=T 0- M3 M3 C— 0- CO in •=r £

M3 on -=r =r t— OO M3 in =r •=T oo CO a- f

• • • • • • • •

* on CM M3 r- in 0- CM in CM o -=T CM O'

C\J <— r— on in o O' in in co O O' o on t—

CM CM

CM «— CM oo M3 =T 0- in CM CM O in in Q CM CO M3 «— 0- O' cm M3 O' in in M3 r— co 0O O M3 O' CO t— r— C— M3 ON CM in co in t— ct— <

r— ro CM on *=3“ CM o

O' £ M>

in

y—

/V Q -=T CM f- lO CO cr» r— on =r co CM in in M3 O C- o Os CM M3 O' m> on CO CM CO CO

to- O' r- O co in ON on co f

O' O' c— cCM -=T on CM on

Q T— O' o O' CM o o O M3 CO O 1 1 1 1 • • 1 • • ' • • • • • • • M3 M3 O CM O' O' o in CO to- O' O' in m3 O on co o i— M3 in E CM *- M3 on CM m CM *- 2

3. o

4) Q O' -=T 4-> in O' 1— in co C" on in in

s: 1 i 1 i • • 1 CO • • • • • • • • ' • on o on onro M3 CM 0- M3 M3 in in co a cm in O' CM t lO CO CM CM

•o on CM r— -=T V— T— y—

a; s_ •a o

r—

<

o O

s <u CO CO CO

4-> CM in in in c ra o 03 JO •3“ in o o o o

o /^s /-N T— c /—

S

'W' T— r— r— O'

CM on in co O' ^ *rH «- w 1 /-•s i /-N, i w ^

CO ' \ 'w' £ N—' [ij w u d: M3 : 0- dC CO

CO CO O CO E— Ci-e Cxj <3 V— CD 0) 'w*’ E- E—

0) a) CLo M3 H s- C_> U. Q -3 O O H E- > > > QC ce

l—f c. d. 1 Ci3 u > > > > 1 1 1 >. >> Cl. a. o. a. cn 2 a. a. 0- a. cl. rH a. w U3 w E- E— H O C-> £ E rH

03 O o • • • • • ' • • • • • • CO o * CM on inio c- cc r- CM m -=r in M3 CO O'

• <c cn

Numbers

in

parentheses

refer

to

samples

prepared

in

Table

Numbers

in

parentheses

refer

to

samples

prepared

in

Table
O'

O O' O' t- CO CO S3 co O' O'

43- v£3 4X o m t- in c— v£3 CM

CM ao M3

CO •k 0 00 00 CO vO t— c~ CM CO

O

OO 00 0 CM 0 O CO in vO r— in 0 E- CM t- O' vO

a •k •> •» • • • 0 in CM in CO rH

T3

05 O' CO O' O' O' 0 vO C*“ CO CO CO CO X cO CO vO in CO 0 O' in CO O' O' ao

05 CO 0

rH •

tJU T“*

t_

COa CO 0 c- CM CO CM M3 CO CM CM t—

05 2: CO =r in 0 C— «=T CM 0 on M3 in H O' 00 in VO O' in C— rH O' O' vO

«k •> « * •k C-, in CM r—

C- 2 O E 0 0 O' c» O' 0 C^5 ZT f— O' CO

•0 CO cm CO CO ST 0 O CO T— CM cQ c r-° 0 CO vO CO r— • 21 05E

05 rH

jo

W T3

44> 0) 0 CO 0 CO O' c- vO 0 CO in O' O' 0 X a 0 CO vO O' vO CM •=r 0 =T c~ vO in c 03 0 0 00 in in 0 vO 0 r— CM O in in

rH «* c_ r— T— CO CO in T— r—

•0 c

05 33 X 0 0 O' CO O' 0 CO vO in O' O' O'

0) CO CM vO vO O' CO O' -=T ao in -=T in

rH O' CO r— CM

U*

CQ T- CM

O CO

O CO 43- CO O' c^- s_ Q C— 0 CM CO c— in O' in in co in vO

0) 2: O' O' in in

O in ao 0 T— 0 O' vO 0. • * • • • *

nj T— in CM CM CM

D_ 0 O' O' CO in vO CO O' CO CM c^ O CO

•H CO in in 0 CO c— T— CO CO CO

-u r— CM f— in T—

05 £

4-> C- in t— t**’ CM O' C- O' CO c Q • >1 O in in in in co C~ 0 •=r -=T co

CO vO C- VO =r in r— CO in c—

m r—=

CM t— CM CM

T3 T3 c 05

ro

X M3 CO t— CO «=r CO M3 CM O' vO r—

0) • 03 rH CO O' 0 vO O' CO c—

— in CO on

05 CXd T“= CM CM -=r r—

4J

03C 05

*»H 05 CO in 0 CO CO vO 0 0 CM O' CO co E 05

(0 c Q =r in CO C- 0 CO 0 in *— M3 in co J 2: M3 CM 0 CO vO t- -=T 0 •=T CO O vO

<L< CM CM «— • r— CM CM CM on

•k 03 4-> E

c. CO • CO 0 vO O' ST in 00 c— O' CO ^T

05 2 CO • a S. 3- O' -=r CO in t~ vO

m C— 0 rr

m 05 r— T— CM CM r— in CO r—

CL >

05 >> rH O' c— CO vO (M T— vO C— CM CM M3 0 •H Q c 4-5 CJ VO 0 CO in 0 CO in CM in CM in VO J3- 05 c O' in vO CO CM on C— vO m O' CM

S- CO T— T—

— CM r— r— CM

c.

O 3

CJ T3

O 0 c— 00 CO

m 0 CO v— CO

05 * •

l-i

X CO O' vO 0 vO in CO CO aom

O 05 *— T— CO co t— r— -3* rH r—

05 Cm

03 c

•H 33 r— 0 in CM •=X O' 0 f— in MD co

m GO

4J • 3 0 r— -ST CM O' O' CM in 0 CM •=T 0 in

05 2: in 0 CM C- 0 in co CM O' M3 a -=r CO t— • t— *— co CM CO on 0

s- 0- •0

05 rH 4-> •0

CO c 05 O 0

°*H 3 c -=r in CM

03

a •H ao 1 1 c- -=r 30 c C. U3 in 0 0 4-> m •C 3 a Q. vO a. 0 T— r— c 1 1 Cl 1 1 Q 1 CL r— -=T X X

a. CL

J 2 co 1 1 | | t_ 05 05 0 0 \ N N 3C X X X 0. C C • 33 CL e- E- E-* H 05 05 05 05 0

t- cc CC CC cc > E E E X

H r—v

CL CL Ou Cl >»

O

O

O 05 05 05 05 C0 0 C5 0 CJ 0 f— 2 2 2 H 2= X rHn • • • <0 • O fB CM

CM CO in vO t— CO ON r-
x>

CO CM N (M CD CO vO

CM C\j Oj ^ CM lO

to m

CM —

tou

^ sr lO CM O' CM lO O

oOOnO*-^CM-»Onno mo^rO*-ojocDO SO

VOro

T3

(1) X

0) UCO

ar

omCM

•a* cm o» o O co to ao co <x> m

cmcm — rn^-^r CM *— ro oj

ON

toro

CMO

O cn o co CO CM CM —

NO

CMO

^CM^^NOCOOOiOO CO cncMcnmr-mmcMCMCM *-

o

X

omcm OCMmmONO'CM — (MOn CMOtOf'OCOO'O'O-3'O' m

O' O' •— «— vo no O to m o

CO CO CM o o

O

0) X

0) Cb

•30 o

oo

a> JO

<TJ fQ

3: C— CO

to f—

CM tO nO f— CO O'

m

o

CO JO

Superscript

numbers

refer

to

samples

In

average.
Table

8.

Mechanical

Properties

of

Currency

Papers,

Laminates

and

Synthetic

Papers

Flexed

In

the

MD o

0)x

as H

Lu

CT3 OS

t. C3Co

CO00co

Cxi

X3

(1) X

as r—4 3c3

COa

cj

coax

COaawax

CO

CM CM CO U'l in -=

n on CM o O o’ o’ O CM — o t— CO

f- 00 o m 'O O' o O ZT • • • • • • • ft ft ft • ft— CM m CO O' m o O' m

CM f- ft— O'

in o o CO in CM CM -=T o • • • • • • • • • • • • o o o o o m CM CM ft— o !

m 3 in oo • ON o o in m 3 O' cn O O' cn on o o CM O' 3 MS cn O MS

CM ft— t"

oom cn CD 3 00 CM CM in in • • e ft ' ft c ft • • • • o o o o O CM ft— ft— o c— 0-

MS ON CD CD on in in CD f- cn oo o

vO . «- CM cn C-= eo cn *= CO ft— CM ft— ft— ON c~-

cn

—

—

— •3” in cn cn

— O' c— o o o o o cn ft— o tMS CD ON ON — o ON cn — O' ft^“ NO cn cn o o o cn as e» CM in ^3* CM ft— ft— o ON

CM ft— cn cn cn

— CM c>-

dd o d

dd o d o o o a

a)x

<u

Cx.

x:4-> 00c

OS S

i.

N

-M> 2

CO SC 00c

•H

CO

OSS. m

•o

asx

0)c3 a ft— in oo o o cn CM CM cn o cn o

cn cn 3 CO MS in NO CM CM cn

O . CM CM

as cn cn cn •=r MS in in ^3* in as O'

co « • o o o d

d o d o o o o o

CM

O C*— CM C—

m cn c— CM O' *3* in 3X C— CO in MS MS CO cn 3 in

CM in

CM CM ft— r— CM oo CM MS CM cn as

CO • o O o o ft— o o o o o o ft— 3 ft- ft- ft— in t- o O 3" m T MS CO O ft ST 3 cn cn MS in NO CM CM cn O'

CM

CO

0.5 0.3 3o0.3 0.7 0.6 0.5 0.6 0.5 6*0 0.7 0.6 3 NO 3* a" o CM ST 3 CO cn CM NO ON CO s • c— OO in NO 00 3- O' 3“ in in

CM NO

•a

cu “O c as

'-t i.

C 3- in c- CM

a as i i 3" c C. Cxi in o o 3“ 4-> m 3 a 3 NO 3 o ft— »— c i 1 1 i 3 i 3 ft— 3- 3" 3" —4 X X

a. 3 3 2 3 i i i i as as o CJ s N N oc X X X 3 c 3 3 H H E- E— as as OS as O —4

cc 05 05 05 > E E E X rH ft4

-C—N

a.a. a. 3 >. o O

O as as as CO O o O o CJ t- 2 2 2 t- s: X

ft o J CM

ft" CM cn 3- in NO t- as O' ft— •— Cft-
Table 8-

continued

(MD

Flex)

-T <— CO r- r— T— o r—

m CM

CO • • » o c o o o o o o o

CO o CM c— in CM CM NO ON 0- in

Q • • • • • • • • • • • O ON o o CM o CM CM o o on •T

r— T—

-3

0)X CM on 0- o CM T— t— CM on

1) co • • • • • • • • • • • rH o o O O o o o o

Uu sr CM cCl • • • • • CM ON NO o ST 0- T— 2 CO CO on in NO

CM o CM on CM T— on •=T

ON o ON 00 on o O CM on on

m co 3 r— o o r— o o o o O

O o

rH3o a CO O' CM sr in ST ST CO ST t— ST OCM 0 £3 2 £ X o CM CO O ON r— o CM CM o r— sr ST N o t— r—

r-l Z i-H 0 o

•H c in t— CM- ON o in r— in on on

4-> co •H r— T— r— o o o o o o o c

HH in NO 1— CO ST in CO in CO ON ON QS NO *—=

on On o on on CM on on

m

CM CM CM

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co

in in ON sr on on on ON NO o

on in c~- ST CM ST oj on on

Q 0 0 U in •— on ON on CO CM CM CO on ON

ST ST on in t— on on 0- NO on •ST NO co ST t— ST ST sr o CM r— ON ST NO T— r— NO ST o0X no on ON ON CM t— o C- o ST CO 0 co • • rH O' CM CM CM ST O in ON ST in CO NO

CX4 T— NO ST o NO T— on T" ' on ST CO 0 0

CM

O on ON f- r— CO o o r—

O in c—

Q2 O on 00 in ON ST CO C- NO in CM on NO

NO CO CM on on ST ON CO sr JT

O on on

r— in in sr CM T— c^ in 0 r— 0

£_ CQ CO t- CM ao in on in in NO CM OvJ ON OCM CM in c- CO c— NO on in ON on 0- ST

4-> 2 on

m c— ON CO on o CM \ on =T

>> -D

SO

£_ 0 05 0 in CO on co CO CM 0- C— o o in sr NO C Q

td o on CO c~ ON in CM CM NO o on T— in NO

•o o CM on on C— r— C~- NO ON co NO o C

— 0 r— CM CM ON on NO r— NO ST X0

r“H CO NO 0- NO o ST c— in ST ON in o

Cw CO • C ctn OJ in ST r— in ST o o o T— CO Z t— NO NO r— 00 CM on on T— CM •T sr 0 0 o O CM on CM in o ON O ON c— on ON QS on o NO •ST on ON CM NO NO on on co CO

in o CM on in ST ON ON r— in CM r— CM NO CO ON CM i— 0- C'- o o0 o c 0

4->

a c ST in CM

CL CO i i c~- ST c s- Cd in o o ST 4-> on sr 3 Cl a. NO Ou o r— T— T— c i i 1 1 Q 1 cu ST ST ST X X

0- a. z CQ i i i i c- 0 0 o o \ \ \ DC X X X CL c c

33 DuH 8- t- E- 0 0 0 0 o H

DC cc cc cc > £ £ £ X rH

DU Du cu a. >>

O o o 0 0 0 0 Q O U o o H z z z H s s , • • • • • O T~ CM

T“ CM on sr in NO CO ON r— r—

Melinex

values
40 o 3J* O' o -ST 40 o 40 OO

co • o CM in

m 04 o o

04 0- o CO o on in CM CM CO CM c- CM o • • o 04 on CO T— O CO in CO 04 O'

7— *— 04 3T -3* on o

(1) X

a) ,

cr> c~- t" CM 0- IT

m -S'

r-H co • • U- o o o o 0- r— t— «— CM CM r— r— T“»

CT3 <D

Q -IT in CM 04 on CM CM CM on CM 2: • <u o o r— CM 3T 40 l>- 40 O' 00 on

04 in -=T 004 W Es o o O' o CO O' O v— in OO

jj co • • o o r— 04 in CM 04 c- CO 40 on

>. CM f—*

to

0.03c Q -=T o 3T 3T *—>

0- on 0- on T—

w

O t— on ao in 40 o o 40 in

04 T— CM on 40 -3“ o

CDX

a) *— r— a- CM CO CM 40 40 04 on 04

pH CO

4-. o o o CM 04 CM on c~ CO c on

2)

Q oo in o -=T O'O 3T in CM 40 CO

z: o o r— in 40 40 CO 40 0- o 04 00 40

T— CM CM

m (M on T— CM CM CM on

CO • • • • o 0 • • • • o O O o O o o O o o o a -3“ CO O CM 40 04 -3" CO on o o o CM o o — *— o — o

03X o r— r— r— CM r— CM CM

0) 00

rH o o o o O o o o O o O

Du

£-

03

Q

m -=T 40 T—

O 04 04 CO 04 o 40

a> z: H E o o o 7— r— o o o o T— 7—

CD 2

M0

•o CM T— CM CM CM *— CM CM *— CM U co O O o o O O o o O o O

40 in o co r— CO

O ^3* 04

Q • • •o CJ O o t— T— r—> o 1 T— T— o r—-

03X

03 T— -3“ CM CM CM CM CM T— CM

CO c o o o O o o O

O

O

OO 2 Q on -=r 40 0- T__ CO o 04 OO =T

z: • o o o o r“ o o a

03 4H o c 03 •H 4-S t- c -3- in CM a •H co 1 i 0- -=T c s_ w in o o 4-> m -3- 3 o. a. 40 a. o «— c i 1 1 1 Q i a. T— =r ^3“ «H X X

cu 0- 2 m 1 i i i (. 03 03 o o s N N X X X Q. c C 2 0- H E— f— t- 03 03 03 03 O •~4 »< cr DC QC a; > E E E X pH

x—N

a. a. 0- a. Sn

O

O

O 03 03 0)

CC3 40 o o CJ) CJ> E- 2 2 2 (- z: z: # . o CM

T— CM

m -=r in 40 0- CO O'
Table

9.

Physical

Properties

of

Currency

Papers,

Laminates

and

Synthetic

Papers

Flexed

in

the

CD o ON 03 O' ON v— c—

m CM f- O' O'

CM in CO 3 on on 3 NO CM in in cn

CO ON

r~ CO 3 r-“

on O' CM ON O' in c— o M3 in CM t- on O NO J— ON t*- 3 o O' CO in M3 O' v£> in 3 c— ON NO in

Q * » •k * «k a 3 on M3 on *“

•o ON ON ON cr> on in CO ao O' O' CO

0) on in in CM 0“m o CO M3 on

X co on CM r— , 0

pHDu

i. o o CO ON O' on CO on o on CO O'

CO 2: o NO in o 1— 3 CM in on 0 in M3 o in ON NO CO o CO NO in H •* » •* T— in CM r—

Cm

s_ z o ON ON C— ON o 3 c— a- O' CO O E co CM on on 3 3 o o on <— 3 CM 0-

-o i— o on NO on c •k 0 1

E

rH

Cd -O

O on ON 00 O' t>- NO r— CO in O' O' o 0) a O on M3 ON NO CM 3 o on C" NO in X o o co in in o NO C~ o T— CM o in in 0 •» * rH r—' r— on on in 3

<l,c3 o ON ON CO ON o on NO in ON ON O'

co CM CO NO O' on ON 3 CO in 3 in 3

O' on CM

CM ON co o CO 3 co c~- ON C—

a C—

O CM ao t- in ON in in CO in NO

s: ON ON in iKO in CO o i— o O' M3 3 k •» «• •k •» r- in CM CM CM

CO ON ON CO CO co co ao O' ON in ao

00 • O' On! 3 co c

c— O' t— CM NO in

CM *-

on c— co NO M3 CM o in in in NO O' cQo c— t*— CO ON O' * O' in NO in O' CM on f— in NO t— O' 3 CM 0- CM VO t—

r— r— r— r— t— r— t» 3 ooX CO CO O' in co NO 3 co CO in CO

0) 1—1

CO ao O' NO on 0- co CO T— CM in r—

Um CM r— CM «— CM t—

cnin

in CM on in O' O' t— c— 3 CM CO o • • c a on on in O' in in 0- c— CO 0- T—

Cu 2: CM 3 co CM 0 0 NO <

on 3 NO . Cu <

r— «— onT CM 3 k— NO t— on

•rH -u E

co • NO O' NO O' 3 in COC

O' CO 3 O' z

C. 3. O>

a>

CO O' 3 co in c

CM 26 e— on 3T 57 0

on

^3“

rH k— O' 0- on NO on «— NO C~- CM •=r CM NO

•H

o>

Q NO NO on in 0 co in CM in CM in NO ^3* c O O' in NO co CM on ^X C— NO -3" on O' CM

to «— *— i— c\i t— cm . 3- r~- -sr CJ

TO 0 O' C' CO on on c- 0 CO C- r— CO

<U • X co O' NO 3“

O NO in on ao CO on 3" t—

CU 3T t

' on on

k

3- T 3" r—

rH r—

Cuc3 0 in CM 3“ O' 0 c— in NO on on CO 0 3T •3“ CM O' O' CM in 0 CM 3“ O in 5: m 0 CM 3“ O' 0 in CO CM O' 3- NO

^X on T— T— T— on r— CM 3“ 1 CO 0- on o0

-d -o c 0

jj

C- c 3- in 0- CM 0. •H co 1 1 C~- 3 c i- U in 0 0 3* cn 3 3 CL CL NO CL 0 T— <

<

c 1 1 1 1 a 1 Cu 3* 3- 3 •H X X

CL CL 3 z CO 1 1 1 1 C. 0 0 O O s \ X X X CL c c 3 CL H H E— H <U <u 0 0 O •*-» *H

QC CE ac CE > E E E X rH rH

CL CL CL CL

O

O

O 0 0 0

<U jOO

O 0 O

H z Z Z E— 2: 2: # O ^ CM t— CM on 3“ in NO 0- CO O' *—
Table

9

-

continued

(CD

Flex)

CO O

CM O o- O

sO m on o co

PM CM fM CM

COO

O

CJ

O

CM

CO (M m ro

00 O'

in o on xr

f— O

on cr> xr m

in on

CO 3

0)K

<D

Cju

O

CMOm

PM

qn^-co*— on in ao in on co

*- pm *- on in in «— *-cm 6— o

'O O' XT O' in co co oSOo

co o

CM — O' —

pm on on

in

CM O nn Om pm CM

co

so

PMO

xrcM^'^'Oaooomoco

oncM m m c^- on on pm cm pm •—

ar

o

on

PM OPMononO'O'PM — PMO>

PMOmoncOCT'CT'O-^'MDon O'Ov — .-vo^-moinmo

CO

Q ON

PJ on

ON

CO on pm O' o

o

o

Lu a

2: O 03

co *0

a) -h o o c u. 3

s. a> 3 ^ 0 n

c 3 u oQ

•oo

u*

O'

O' O'

in on

o o o in — pm — o

on

O'

c—

CO -S' CO o

CO m

H»-h r

*3

0)X

0)c3

CO

0

2: o

PM on in md CO O'

X

n

D

3

Superscript

numbers

refer

to

samples

In

average.
Table

10.

Mechanical

Properties

of

Currency

Papers,

Laminates

and

Synthetic

Papers

Flexed

in

the

CD o o o II co

on on on on on O O O on c\j

on NO ON ON NO c- CO CO on -=T i CM

Q • i CJ =r NO *— T— CM 00 00 m r— CO i CO

CM •- •— in c

0) o o r—m NO CM r— CM =r CNJ

X cn • <D o o o o *— r— r— o NO CO

rH

Lt- CO ON o r

_ on •3* on NO NO ON

Q • z: o o r— r— -=r o NO on ON NO

CM O' O'

re CO

m -=r on OO -=T CO CM CM

—

in un

CD CO • • s_ ao

4-5 o o o o o CM o c— C Q NO ON ao CO on in in CO r— on CO -=T o O W CJ

**H 4J

rebOc

=r NO CM on C—

CM CO on

—

OO ON c- o -o on r— r— r— O -=r in on on ON c

r-t CD CO • Cd X

CD rH o o o o O on o C— C— c •=r NO CO CTN ON t— o ON on <

ON r— NO

aa

z: on on o o o on

C\J CO c— CM ino

=r

on t— r— on r— CO CM CM CM =X 1 o

co • • o o o o o o o O O O 1 <—

•o

0)X

CD rH

Du

a ON o r— -3“ -=r NO CM CM on on NO i in o | • on -=r on on .=T in NO in NO CM CM 1 CO

on on CM in in •=r .=r =r ON c- NO o o O o o o o o o o o

jz

4-5 bOC

CD E

S- \

4-5 2

00 ^

COc

03

a>

s_ a

a

cdx

0) r—t ca

NO o CM ON NO ON r— ON on in ON

a

z: in NO c— CO •=r CO =r •=x in

CM NO

CM CM 1 r— CM CO CM NO CM on CO ,

CO • o O o o * o O

OO o o *

QO

COQ

ZI

N- Nn 0- o o -=r on -=r NO co

-=X on on to- NO

n NO CM CM on ON

CNJ

n on =X on C—

n NO

n ON c— NO o o o o O o o o o o o o

NO -=r •=r o On) •=r ^=r co on CM NO ON co

c— CO

n iO 0- co -=X ON .=rn

n

CM NO

T3

<D

4-5 "O C CD —I 4-5 s. c 3T

n co- CM o. •H CO 1 i h- •3" c c. Cd n o o =T 4-> ere -3- 3 a 0. NO a. o 1

.

i

c i 1 1 i Q 1 D- T— 53- 3“ -3- —t X X

O. 0-

J 2 m i 1 | 1 £_ CD (D o o Ny s s X X X a C C a 0u H t- E- E- CD CD CD CD o •H -4

CE ce CE CE > E E E X rH rH *—s /—V

Q» Cu Q. 0- :n

O

O

O CD CD CD

re o o u

O o E- 2 2 2 E— z: z:

CNJ LPi NO CO CTN

O CM
X

0)

r-l

Cx- au

cm O' -=r vO

m

m O' rr in in

CO • • o o <—

m C\J

m

m CO CO CO

Q c- (M v£> CO on t- in r- on O' on

C_3 • o CM

m in o 'O CM o r— Q\ 0-

r- T— CM ^Tm

m

to

a>X

4) o r— M3

m CO 6- CO O' in CO

rH CO • • Lu o o o r— V—

T *— in M3 c—

t_

CtJ a> E- CCO m in o CO on CO 0- on C— *— .T 3: • • • 0) o o r— a- O' in M3 •T in •=X 60 r— tt .

it

TO

CiX\|c o \ O' IT o CO O' o in 00 0-

4-> -S CO o o *—=

CM in CM CM C"* CO M3 on

3>> CM r60

l.

43c a IT o •=T it T“ 0- on c— on *— w o • V— *— m CO in M3 o o M3 o in

CM CM on M3 •=r TO

0)X

a; T— r— CM CO CM M3 M0 O' on o

rH CO • 4-, o o o CM c

r— CM CM on 0- 00

C on 3 Q on in o •3“ O' O TT in CM M3 oo 2 • • o o f— in M3 iO CO M3 0- o

CM CO M3

CM CM on CM CM CM t— CM T—

oo • • o O

O o o O

O o O o o Q IT CO O CO M3 CO r- t— it 0- t— O • o o O o *“ o

TO

43X r— T— r— CM r—»

CM CM r— on r— CM

03 CO

rH o o o o o O

O o o o O

Cx* -

i. o

03

Q on in COM3 O' OO CM CM CM

d) 2 H £ o o o T— o o O T— r— o *—

(0 2

60 0C •o CM T— CM TT CM CM T— *— CM CM CM W CO o O o o o O O O O O O M3 in o CO r— OO r— o :t O' r— a T3 o o o T— 4— o T— *— r— o r—

03X

43 rH r— T— IT CM CM CM CM oo V— CM 4- CO c o o O o O O O O o o o 3 a on IT M3 0- CO O O' CO IT 2 o o O r— o 1— o *— o r— 3 4-5 TO c c 43 «H •H 4-> 4-3 S- c un 0- CM c a •H CO i l Z3" o c s_ Cd in o o 4-> m IT o 3 a CL M0 Cl o T— *— •— c i 1 1 i Q 1 Cl T— rr IT •H X X 1 CL CL -3 2 CQ 1 i 1 | 03 03

C-3

O S \ \ oc

XX

X a. c C o 33 CL E- H E- E— 43 03 43 43 o

r— CE OS cc cc > E E E X

H rH

«r-»v CL CL CL a. >.

OOO 43 43 43

43 (0 30 o o CJ o E- 2 2 2 E- 2 2 rH

30 • • • CO • O CM

E— r— CM

m -=r in MD t~ CO O' •—
These

Mellnex

values
U.S. 3EPT. 3P C 3mm. 1. PLBL cat dn or REPORT NO.

2. Performing Organ. Report No. BIBLIOGRAPHIC DATA

SHEET See nstmctions) MBS IR—84-2951

3. Publication Tate

November 1984

4. T TLE AND SU 3TITLE

The Testing of Laminates and Synthetic Papers as Currency Substrates

5. AUTHOR(S)

W. J. Pummer, E. E. Toth-Debelius , F. W. Wang

6. PERFORMING ORGANIZATION : * joint or other than N3S. see in structicn s)

national bureau of standards

DEPARTMENT OF COMMERCE

WASHINGTON, D.C. 20234

7. Contract/Grant No.

S. Type of Report & Perioa Covered

9. SPONSORING ORGANIZATION NAME AND COMPLE i E ADDRESS Street, Office of Research and Technical Service

Bureau of Engraving and Printing

Department of the Treasury

Washington, DC 20220

ity. State, Z 3

10. supplementary notes

Document describes a computer program; SF-135, = ':PS Software Summary, is attacned.

11. ABSTRACT A 200-word or ess factual summary of most Significant information. If document nc ,tes a s g- f cent

bi bl lOgraphy or literature survey, mention it here) The cost of maintaining an adequate supply of currency could be significantly re- duced by increasing the circulation lifetime. The principal factor controlling

lifetime is the deterioration of the mechanical properties, particularly flexure,

of the currency substrate. It is well-known that synthetic polymers, either as coatings or laminates, can improve the flexure properties of paper. Also an entirely synthetic polymer substrate would be expected to result in a more durable

currency. In addition to the choice of coatings or laminates there are a large

number of synthetic polymers that may be suitable materials. Thus, the task of

identifying a suitable system for currency is formidable without further selection

criteria. We present here the final report of our joint effort with the 3ureau

of Engraving and Printing to develop such selection criteria.

12. KEY WORDS S x to twelve entries; alphabetical order; capita ze oniy crape' - z~es; arc sepc'Ote <e. Currency paper; laminates; physical and mechanical properties; synthetic papers

13. AVAILABILITY ~ U nl i mi ted V For Official Distribution. Do Not Release to NT'S

Order From Suoerin tenaent o

? Documents, U.S. Cover"- ent P 'in ting Of* ce. ” asr - gtc •- D.C. 20402.

Order F-om National Technical Information Serv.ce NT'S . Soring* eid, VA, 21 ?

14. NO. OF

B RiNTED Pi

15. P'