######### Appendix B

**Table of Contents**

B1. OVERVIEW B-[2](#b1.-overview)

B2. MATERIALS REVIEW PROCESS B-[2](#b2.-materials-review-process)

B3. LIST OF CANDIDATE MATERIALS B-[2](#b3.-list-of-candidate-materials)

**List of Figures**

Figure B.1 Non-Metallic Materials Identification And Usage List
B-[11](#__RefHeading___Toc456750296)

Figure B.2 GSFC Spacecraft Inorganic Materials List
B-[12](#__RefHeading___Toc456750297)

Figure B.3 GSFC Spacecraft Polymeric Materials List
B-[13](#__RefHeading___Toc456750298)

Figure B.4 GSFC Spacecraft Lubrication List
B-[14](#__RefHeading___Toc456750299)

Figure B.5 GSFC Spacecraft Materials Processes List
B-[15](#__RefHeading___Toc456750300)

Figure B.6 Material Usage Agreement Form
B-[16](#__RefHeading___Toc456750301)

List of Tables

Table B.1 Materials List Enclosure MSFC-SPEC-522B Attachment A
B-[4](#__RefHeading___Toc456750302)

Table B.2 Materials with Low Outgassing and Flammability Data Available
B-[7](#__RefHeading___Toc456750303)

**Appendix B**

**Material**

# B1. OVERVIEW

As part of the System Safety Process, GSFC Materials Engineers review
all materials used in HH payloads for freedom from stress corrosion
cracking and to determine their potential flammability, toxicity, and
offgassing^1^ characteristics. Materials are also reviewed to determine
their outgassing^2^ and contamination characteristics so that scientific
data degradation is minimized. (Note: A good rule to follow in meeting
materials requirements is to house hardware in sealed containers).

# B2. MATERIALS REVIEW PROCESS

a\. Complete the appropriate forms applicable to your payload at a
relevant point in the design process.

> b\. Submit completed forms to the HH Project Office, which will
> forward them to the HH Materials Engineer for review.
>
> c\. If any questions arise during the Materials Engineer\'s review,
> you will be contacted by telephone.
>
> d\. The Materials Engineer will document his findings at the
> completion of his review and forward them to you through the HH
> Project Office.

(Note: Some findings may require the submission of a material sample for
test by GSFC or recommend an alternate material for one that is
unacceptable for use.)

1\. Offgassing - The emanation of volatile matter of any kind from
materials into a manned pressurized volume.

2\. Outgassing - The emanation of volatile materials under vacuum
conditions resulting in a mass loss and/or material condensation on
nearby surfaces.

# B3. LIST OF CANDIDATE MATERIALS

For the immediate needs of the HH and SPOC, we have generated lists of
materials which, if used prudently, can form the basis of an acceptable
materials design. It should be noted that while the materials listed are
considered \"acceptable\" for space use, successful performance is not
ensured without having an appropriate technical merit review by
materials engineers. Nor does it assure that the selected material will
not be used improperly.

This selection was based on certain criteria for polymers and metals in
light of the referenced documents. Limitations regarding outgassing of
polymers and the stress corrosion cracking of metals are of major
concern to Shuttle payloads. In addition, test results such as
flammability may not be readily available in the manufacturers\'
literature and may require further testing at JSC.

It is required that the selection of materials used in the design of
payload structures, support brackets, and mounting hardware complies
with the stress corrosion cracking criteria of the latest version of
MSFC-SPEC-522. Acceptable materials taken from MSFC-SPEC-522B are given
in Table B.1. Other materials need to have a Materials Usage Agreement
(MUA) submitted for approval.

Refer to NASA Ref. Pub. 1124, August 1987, for lists of materials which
have been tested for outgassing and have met the acceptable criteria.
This criteria is that a maximum 1% Total Mass Loss (TML) and a maximum
of 0.10% Collected Volatile Condensable Materials (CVCM) is acceptable.
For materials that are not included, the Materials Branch of the GSFC,
Code 313 should be contacted to determine their outgassing values.

Wherever more stringent outgassing criteria are needed, such as near
sensitive optics, the CVCM value of 0.01% should be used. A list of
these materials is included in Table B.2. Most of these materials will
cure at room temperature and those that require an elevated temperature
cure are indicated by an asterisk (\*). In addition, those materials
considered to be \"non-flammable\" per JSC/White Sands Test Facility
(WSTF) data are indicated by a (1).

In using materials for space flight applications, several general
precautions should be considered:

a\. The use of electroless nickel on flexible members is not recommended
due to its brittle nature.

b\. Metal platings used as a corrosion protection film, should be at
least 200 x 10-6 inches thick.

c\. When the recommended Brayco oil and greases are used, a barrier film
should be properly applied for prevention of lubricant creep.

d\. The use of Ray Chem Spec 44/ or 55 wire is not prohibited, although
it is classed as flammable. It is highly recommended that Teflon TFE
(MIL-W-22759/11-12) or Kapton polyimide (MIL-W-81381/9-12) be used
throughout the Program. Neither are flammable.

e\. When using dry solid film lubricants and metal platings, allowance
must be made for the lubricant thickness. Sputtered MoS2 does not change
the dimension to any significant degree.

f\. Formulate plans for controlling the particulate and Non-Volatile
Residue (NVR) contaminants around optics.

g\. Use care in mixing and curing polymeric materials.

h\. Use proper identified and dated (shelf life) materials at all times.

i\. Use the proper primer with paints, conformal coatings, and potting
compounds.

j\. Flammability data is available on a limited number of materials as
shown in Table B.2.

As a final note, these attached lists should be considered as a starting
point and do not negate the use of other materials. It is not the intent
of these lists to limit the use of materials to a select group but
rather to assist the customer by listing those which have been used in
previous space projects. Selected materials should be submitted for
approval through the project office on forms shown in Figures B-1
through B-6.

[]{#__RefHeading___Toc456750302 .anchor}Table B.1 Materials List
Enclosure MSFC-SPEC-522B Attachment A

Alloys With High Resistance To Stress Corrosion Cracking

####### STEEL ALLOYS

[Alloy]{.underline} [Condition]{.underline}

Carbon Steel (1000 Series) Below 180 ksi UTS

Low Alloy Steel (4130, 4340, D6AC, etc.) Below 180 ksi UTS

Music Wire (ASTM 228) Cold Drawn

1095 Spring Steel Tempered

HY 80 Steel Tempered

HY 130 Steel Tempered

HY 140 Steel Tempered

ASP 11 Aged

200 Series Stainless Steel (Unsensitized) (1) All

300 Series Stainless Steel (Unsensitized) (1) All

400 Series Ferritic Stainless Steel (404, 430, 444, etc.) All

Nitronic 32 (2) Annealed

Nitronic 300 (2) Annealed

Nitronic 40 (formerly 21-6-9) (2) Annealed

A-286 Stainless Steel All

AM-350 Stainless Steel SCT 1000 and Above

AM-355 Stainless Steel SCT 1000 and Above

AM-362 (Almar 362) Stainless Steel 3 Hrs. at 1000oF

Carpenter 20Cb Stainless Steel All

Carpenter 20Cb-3 Stainless Steel All

Custom 450 Stainless Steel H1000 and Above

Custom 455 Stainless Steel H1000 and Above

15-5PH Stainless Steel H1000 and Above

PH15-7Mo Stainless Steel CH900

17-7PH Stainless Steel CH900

\(1\) Including weldments of 304L, 316L, 321, and 347

\(2\) Including weldments.

[ALUMINUM ALLOYS]{.underline}

[WROUGHT]{.underline} [CAST]{.underline}

######## ALLOY (1) TEMPER (2) ALLOY (3) TEMPER 

1000 Series All 319.0, A319.0 As Cast

2011 T8 333.0, A333.0 As Cast

2024 Rod, Bar T8 355.0, C355.0 T6

2219 T6, T8 356.0, A356.0 All

2618 T6 357.0 All

3000 Series All B358.0 (Tens-50) All

5000 Series All (4), (5) 359.0 All

6000 Series All 380.0, A380.00 As Cast

7049 T73 514.0, (214) As Cast

7149 T73 518.0, (218) As Cast (5)

7050 T73 535.0 (Almag 35) As Cast

7075 T73 A712.0, C712.0 As Cast

7475 T73

\(1\) Including weldments of the weldable alloys.

\(2\) Including mechanically stress relieved (TX5X orTX5XX) tempers when
applicable.

\(3\) The former designation is shown in parenthesis where significantly
different.

[Table B.1 (Cont'd)]{.smallcaps}

\(4\) High magnesium alloys 5456, 5083, and 5086 should be used in
controlled tempers (H111, H112, H116, H117, H323, H343) for resistance
to SCC and exfoliation.

\(5\) Alloys with magnesium content greater than 3.0 percent are not
recommended for high temperature application, 66oC (150oF) and above.

Condition

CDA No. (1) (% Cold Rolled) (2)

110 37

170 AT, HT (3)

172 AT, HT (3)

194 37

195 90

230 40

422 37

443 10

510 37

521 37

524 0

606 0

619 40 (9% B phase)

619 40 (95% B phase)

638 0

655 0

688 40

704 0

706 50

710 0

715 0

725 40

752 50

\(1\) Copper Development Association alloy number.

\(2\) Maximum percent cold rolled for which SCC data is available.

\(3\) AT - Annealed and precipitation hardened.

HT - Work hardened and precipitation hardened.

[Table B.1 (Cont'd)]{.smallcaps}

[NICKEL ALLOYS]{.underline}

[Alloy]{.underline} [Condition]{.underline}

Glass Seal 52 CR (51Ni-49Fe) All

Invar 36 (36Ni-64Fe) All

Hastelloy B Solution Heat Treated

Hastelloy C All

Hastelloy X All

Incoloy 800 All

Incoloy 825 All

Incoloy 901 All

Incoloy 903 All

Inconel 600 (1) Annealed

Inconel 625 Annealed

Inconel 718 (1) All

Inconel X-750 All

Monel K-500 All

Ni-Span-C 902 All

Rene\' 41 All

Unitemp 212 All

Waspaloy All

####### MISCELLANEOUS ALLOYS

Alloy Condition

Beryllium S-200C Annealed

HS 25 (L605) All

HS 188 (1) All

MP 35N Cold Worked and Aged

MP159 Cold Worked and Aged

Titanium 3A1-2.5V All

Titanium 5A1-2.5SN All

Titanium 6A1-4V All

Titanium 10Fe-2V-3A1 All

Titanium 13V-11Cr-3A1 All

Titanium IMI 550 All

Magnesium M1A All

Magnesium LA141 Stabilized

Magnesium LAZ933 All

\(1\) Including weldments

[]{#__RefHeading___Toc456750303 .anchor}Table B.2 Materials with Low
Outgassing and Flammability Data Available

MATERIALS WITH LOW OUTGASSING AND FLAMMABILITY DATA AVAILABLE

######## ADHESIVES, CONFORMAL COATINGS (C.C.) AND POTTING COMPOUNDS

Armstrong A-12; 3A/2B epoxy(1) adhesive

Armstrong A-31; 6A/4B epoxy(1) adhesive

Epon 828/TETA; 10A/1B epoxy(1) adhesive, C.C.

Epon 828/Versamid 140; 70A/30B epoxy(1) adhesive, C.C.

Hysol 11C; 1A/1B epoxy adhesive

Crest 3135/7111; 1A/1B epoxy adhesive

Stycast 2850/Cat. 9; 10A/0.3B epoxy adhesive

Stycast 2057/Cat. 9; 100A/6B epoxy potting

Stycast 2651MM/Cat. 9; 100A/6.5B epoxy adhesive, potting

Hysol C2-4259/3401 epoxy potting

Conathane EN21; 100A116B polyurethane adhesive, C.C., potting

Uralane 5753LV; 1A/5B polyurethane C.C., potting

Solithane 113/300 Formula #4 or #21 polyurethane C.C., potting

P.R. 1660L; 25A/100B/8 Cab-0-Sil polyurethane adhesive, potting

DC93500; 10A/18 silicone adhesive, potting, C.C.

RTV 566; 0.1% Cat. silicone adhesive, potting, C.C.

RTV 567; 0.5% Cat. silicone adhesive, potting, C.C.

RTV 142 silicone adhesive

######## WIRE AND CABLE WITH TEFLON 

(MIL-W-22759/11; MIL-W-22759/12) or Kapton polyimide

MIL-W-81381/9-12 (1)

######## SHRINK TUBING

Chemfluor Teflon\* (1)

ThermoFit 400 Teflon\* (1)

ThermoFit TR218 Kynor/Viton\* (1)

ThermoFit TFE-R Teflon\* (1)

######## ELECTRICAL CONNECTORS/FEEDTHROUGHS

AMP-Feedthrough term block 204307-6-70-39 epoxy

Appleton Connector Red/Black Phenolic/Fiberglas

Bendix Connector PT07H-14-19P Green

Cannon Connector MS3476 Black Phenolic

Cannon Connector C-16 MS C-40M 39569 silicone

Cannon Connector PV6G24831/SWC16 Red silicone

DAP Connector Insert DDM 24W7P

Deutsch Connector 6825 RM04-4428 silicone

[ELECTRICAL SHIELDS]{.underline}

Eccosorb MF112 Fe filled epoxy

Eccosorb MF113 Fe filled epoxy

Cho-Seal 1217 Ag filled fluorosilicon 125\*

Cho-Seal 1221 Ag filled silicone aerospace 200\*

######## FILM AND SHEET MATERIALS

Cellulose acetate butyrate 200 micron purple film

Cronar polyester transparency film

Genotherm HT unplasticized PVC clear film

Mylar LA616 film

Kapton H-film (1)

Polychrome 8 mil film

Tedlar 150-30 CC black film

Ormalon TG 4030 neutral Teflon or glass cloth-heat barrier film

Beta Marquisette woven fiberglass,Style 2530

Fairprene VS0080 black Viton A sheet (1)

Fluoroglas 389-7 beta cloth/PTFE coated (1)

Cho-Therm 1677 white fluorosilicone-thermal control

Dacron mesh E2A polyesternetting - thermal blanket

Dacron mesh 15320 polyester netting - thermal blanket

G401500 Ag/Teflon film (1)

######## FOAMS

P-65 polyether urethane foam white methyl alcohol wash

Absafil F1200/20 glass fibers

Skybond R1 7271-12 or 18 rigid polyimide

Zerefil F700 vinyl/20 glass fibers

Scott polyester urethane 100 TPI methyl alcohol wash\*

######## LUBRICANTS

Brayco 815Z oil (1)

Brayco 601, 602, and 603; RP, MS and Zn grease (1)

Apiezon L and N; grease

Rulon A,B,C,J,LD and 123; Teflon/fiberglass solid

MoS2 -filled vespel grade, SP3

######## THERMAL INTERFACE CONTROL MATERIALS

Eccobond 57C; 1A/1B, Ag filled epoxy adhesive

Hysol K-16; 3A/1B, epoxy adhesive

Cho-Therm 1677 white fluorosilicon\* (1)

Cho-Therm 1671 white silicone\*

G-9042 white silicone thermal grease (1) (2)

G9052 black silicone (2)

BrayCo 3L-38-Zn fluorocarbon grease (1) (2)

McGhan NVSIL 2946, two part silicone

McGhan NVSIL CV2942

Eccosil 4954

######## FACING TAPE AND CABLE TIES

Stur-D-Lace 18DH - scoured

Temp Lace 230 Teflon (1)

Ty-Rap Ty25M Tefzel (1)

Ty-Rap Ty307 Teflon

Velcro midtemp Nomex polyimide fastener

TABLE B.2 (Cont\'d)

CIRCUIT BOARDS

Nema G-10 Mica/Cell55 (RCA)

Micaply PG 418T polyimide fiberglass (MCA) (1)

602 Teflon/fiberglass (ATL) (1)

Duroid 5870 Teflon/fiberglass (ROG) (1)

Duroid 5880 Teflon/fiberglass (ROG) (1)

Multilayer board - MIL-P-55617, 55636, 13949

######## LAMINATES

\*Hercules 2002 M graphite fiber reinforced polyers, GFRP

\*Gy70/X-30 GFRP (1)

\*Gy 70/5208 orGy70/5209 GFRP (1)

Hexcel-F174-120 glass cloth/polyimide prepreg.

KG098 Teflon/fiberglass (MMM)

Narmco 8517 epoxy/glass

T300/934 GFRP (1)

######## LABELS AND MARKING INKS

Scotchcal 8001 and 8009 - aluminum labels (3M)

Scotchcal 8005 photosensitive film (3M)

Wornow Cat-L-Ink 50-100/Cat. 9/50-900 white

######## MOLDING COMPOUNDS

Acrylafil G47/20 styrene/acrylonitrile/fiberglass

AF 1006 acryl butadiene styrene

CF 1006 styrene/fiberglass

Dapon M - C2580-11B FR-FMC

DF 1006-polycarbonate/fiberglass

GF 1006-polysulfone/fiberglass

JF 1006-polysethersulfont/fiberglass

Lexan 500-polycarbonate

Noryl EN26

Stycast 0005 polystyrene (1)

Teflon PFA-TE 9704 (1)

Tefzel (1)

Vespel SP-5 polyimide/glass fiber (1)

######## PAINTS

Chemglaze Z306 black (1)

GSFC - 01550 white resin/ZRO

RTV 602 Dev. 764-1A white (GSFC) (1)

######## RUBBERS/ELASTOMERS

ECD 006 and 487-90 perfluoroelastomer (1)

Fluron FS005 Viton red (1)

Gor-Tex carbon doped expanded Teflon (1)

Kalrez 1050 or 3018 perfluoroelastomer (1)

Mosites 1059 Fluorel fluoracarbon (1)

Parker O-Ring S-383-70 red silicone

Parker O-Ring V-747-75 Viton E6G (1)

Viton B

######## TAPES

3M 415 Scotchpar - 2 sided

3M X-1255 Kapton - 2 sided\*

3M Y-9460 Kapton transfer

3M Y-967 Kapton transfer

G400201 A1/Teflon (1)

G406400 A Kapton (1)

3M Y9339 A1 flil (1)

3M 420 Lead foil (1)

3M 425 Al foil (1)

3M 5 polyester

Mystik 7375 Tedlar (1)

Mystik 7420 Copper foil (1)

Temp-R-Tape Kapton (1)

NOTE: (1) - Considered non-flammable per JSC/WSTC data.

\* - Other than Room Temperature (RT) cure.

\(2\) - Migrates when heated sufficiently.

![](media/image1.png){width="5.932638888888889in"
height="8.702083333333333in"}

[]{#__RefHeading___Toc456750296 .anchor}Figure B.1 Non-Metallic
Materials Identification And Usage List

![](media/image2.png){width="5.684027777777778in"
height="8.595833333333333in"}

[]{#__RefHeading___Toc456750297 .anchor}Figure B.2 GSFC Spacecraft
Inorganic Materials List

![](media/image3.png){width="5.617361111111111in"
height="8.702777777777778in"}

[]{#__RefHeading___Toc456750298 .anchor}Figure B.3 GSFC Spacecraft
Polymeric Materials List

![](media/image4.png){width="5.956944444444445in"
height="8.801388888888889in"}

[]{#__RefHeading___Toc456750299 .anchor}Figure B.4 GSFC Spacecraft
Lubrication List

![](media/image5.png){width="5.05625in" height="8.498611111111112in"}

[]{#__RefHeading___Toc456750300 .anchor}Figure B.5 GSFC Spacecraft
Materials Processes List

<table style="width:100%;">
<colgroup>
<col style="width: 15%" />
<col style="width: 3%" />
<col style="width: 4%" />
<col style="width: 6%" />
<col style="width: 15%" />
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<col style="width: 6%" />
</colgroup>
<tbody>
<tr class="odd">
<td colspan="12"><p><strong>MSFC-SPEC-522B</strong></p>
<p><strong>APPENDIX B</strong></p></td>
</tr>
<tr class="even">
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td>C</td>
<td colspan="3">USAGE AGREEMENT NO.:</td>
<td>REV.</td>
<td colspan="2" rowspan="4">PAGE OF</td>
</tr>
<tr class="odd">
<td colspan="5">MATERIAL USAGE AGREEMENT</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td rowspan="2"></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>PROJECT:</td>
<td colspan="2"></td>
<td></td>
<td>SYSTEM:</td>
<td colspan="2">SUBSYSTEM:</td>
<td colspan="2">ORIGINATOR:</td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
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<td></td>
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</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td></td>
<td rowspan="2"></td>
<td rowspan="2"></td>
<td></td>
<td></td>
<td rowspan="2"></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td colspan="4">PART NUMBER(S)</td>
<td colspan="2">USING ASSEMBLY(S)</td>
<td colspan="3">ITEM DESCRIPTION</td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
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<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td colspan="2"></td>
<td></td>
<td rowspan="2"></td>
<td rowspan="2"></td>
<td></td>
<td></td>
<td rowspan="2"></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td colspan="4">MATERIAL DESIGNATION</td>
<td colspan="2">MANUFACTURER</td>
<td colspan="3">SPECIFICATION</td>
</tr>
<tr class="odd">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td rowspan="2"></td>
<td rowspan="2"></td>
<td rowspan="2"></td>
<td></td>
<td></td>
<td rowspan="2"></td>
<td></td>
</tr>
<tr class="odd">
<td colspan="5">MATERIAL CODE</td>
<td colspan="2" rowspan="2">LOCATION</td>
<td rowspan="2">ENVIRONMENT</td>
</tr>
<tr class="even">
<td>THICKNESS</td>
<td colspan="3">WEIGHT</td>
<td>EXPOSED AREA</td>
<td colspan="2">HABITABLE 0</td>
<td>PRESSURE PSIA</td>
<td>TEMPERATURE of</td>
</tr>
<tr class="odd">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td colspan="2">NONHABITABLE 0</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td rowspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td colspan="3">APPLICATION</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
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<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
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<td></td>
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<td></td>
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<td></td>
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<td></td>
<td></td>
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</tr>
<tr class="odd">
<td></td>
<td colspan="2"></td>
<td></td>
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<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
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<td></td>
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<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>RATIONALE:</td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
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<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td rowspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td rowspan="2"></td>
<td rowspan="2"></td>
<td></td>
</tr>
<tr class="odd">
<td colspan="3">ORIGINATOR:</td>
<td></td>
<td></td>
<td colspan="3">PROGRAM MANAGER:</td>
<td></td>
</tr>
<tr class="even">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td colspan="12">MATERIALS APPLICATIONS EVALUATION BOARD
DISPOSITION</td>
</tr>
<tr class="odd">
<td></td>
<td colspan="2"></td>
<td></td>
<td>DATE</td>
<td colspan="2">APPROVE</td>
<td>REJECT</td>
<td>DEFER</td>
<td colspan="2">MAEB MEMO NR.</td>
<td></td>
</tr>
<tr class="even">
<td>CHIEF:</td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td>SECRETARY:</td>
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td colspan="2">EFFECTIVITY</td>
<td></td>
</tr>
<tr class="even">
<td colspan="3"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="odd">
<td colspan="2">REMARKS:</td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td colspan="2"></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
</tbody>
</table>

[]{#__RefHeading___Toc456750301 .anchor}Figure B.6 Material Usage
Agreement Form