Critical Velocity 

of Electromagnetic Rail Gun 

in Response to Projectile Movement 

by Jerome T. Tzeng 

ARL-TR-2794 August 2002 

Approved for public release; distribution is unlimited. 
NOTICES 

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The findings in this report are not to be construed as an official Department of the Army position 

unless so designated by other authorized documents. 

Citation of manufacturer’s or trade names does not constitute an official endorsement or approval 

of the use thereof. 

Destroy this report when it is no longer needed. Do not return it to the originator. 
Army Research Laboratory 

Aberdeen Proving Ground, MD 21005-5069 

ARL-TR-2794 August 2002 

Critical Velocity 

of Electromagnetic Rail Gun 

in Response to Projectile Movement 

Jerome T. Tzeng 

Weapons and Materials Research Directorate, ARL 

Approved for public release; distribution is unlimited. 
ii

Abstract 

A model is developed to investigate the dynamic response of an electromagnetic rail gun 

induced by a moving magnetic pressure during launch of projectiles. As the projectile velocity 

approaches a critical value, resonance can occur and cause high-amplitude stress and strain in 

the rail at the instant and location of the projectile’s passage. In this study, governing equations 

of a railgun under dynamic-loading conditions are derived that illustrate a lower-bound critical 

velocity in terms of material properties, geometry, and barrel cross section. A study is then 

performed to show the effect of these parameters on the critical velocity of the barrel. 

Accordingly, the model that accounts for projectile velocity and gun construction can be used to 

guide barrel design. 
iii

Contents 

List of Figures v 

List of Tables vii 

1. Introduction 1 

2. Analysis 1 

3. Numerical Results 5 

4. Conclusions 8 

5. References 9 

Report Documentation Page 11 
iv

INTENTIONALLY LEFT BLANK.
v

List of Figures 

Figure 1. A schematic of the EM gun cross section, rail, and loading conditions. ........................2 

Figure 2. Coordinates system and model simulation......................................................................2 

Figure 3. Modeling of containment stiffness. .................................................................................5

Figure 4. Effects of the rail thickness on the critical velocity. .......................................................6 

Figure 5. Effects of the containment thickness on the critical velocity..........................................7 

Figure 6. Effects of the rail material properties on the critical velocity.........................................7 
vi

INTENTIONALLY LEFT BLANK.
vii

List of Tables 

Table 1. Mechanical properties and geometric parameters of the rail and containment. ...............5 
viii

INTENTIONALLY LEFT BLANK.
1

1. Introduction 

A strain of very high amplitude and frequency, commonly referred to as dynamic strain 

amplification, develops in a conventional gun tube at the passage of the projectile. The 

phenomenon is caused by the resonance of flexural waves when the moving pressure approaches 

the velocity of wave propagation in the gun tube. The resonance response in an isotropic 

cylinder attributed to a moving pressure load has been investigated by Taylor [1], Jones and 

Bhuta [2], Tang [3], and Reismann [4]. Simkins [5] investigated the dynamic response of 

flexural waves in steel gun tubes, as very large strains have been observed in a 120-mm tank gun 

barrel. Hopkins [6] applied finite-element analysis to obtain a solution in a more complex taper 

geometry. Tzeng and Hopkins [7] investigated the dynamic strain effect in cylinders made of 

fiber-reinforced composite materials overwrap with a metal liner. Tzeng [8] extended the 

research to study fracture in the composite gun tube due to the dynamic response. 

In this report, an analytical solution was developed to obtain the critical velocity of an 

electromagnetic (EM) rail gun barrel attributed to dynamic-loading conditions. Dynamic 

response could be a concern, particularly when a fieldable EM barrel has to be of lightweight 

construction with a hypervelocity launch capability. Figure 1 shows a schematic of an EM rail 

gun cross section and loading condition [9]. The rail and insulator (typically ceramic or polymer 

composite) were contained and supported by a containment structure. The rails are in 

compression due to the EM force acting on the rail and reaction force resulting from the 

containment structure. Furthermore, the magnetic force in the rail is discontinuous at the 

location of projectile armature where the electrical current passes through. The discontinuity of 

the force causes a local-bending moment and shear stress in the rails near the armature location. 

The pressure front will move along the rails as the projectile moves down through the barrel. 

Accordingly, dynamic stress and strain occur as the projectile movement approaches the critical 

velocity of the railgun. 

2. Analysis 

Consider a railgun cross section, as shown in Figure 1. The rail has a rectangular cross section 

and is mechanically supported by a rigid insulation and a containment structure [10]. The 

structural response of the rail can be modeled as a beam sitting on an elastic foundation, as 

shown in Figure 2. Accordingly, the rail is the beam and the support from the insulation 

material and containment is modeled as an elastic foundation. It is assumed that structural 

interaction between the rail and the containment is modeled through the elastic constant. The 

magnetic 
2

Figure 1. A schematic of the EM gun cross section, rail, and loading conditions. 

Figure 2. Coordinates system and model simulation. 

EM Pressure

Projectile 

Rail 

Insulation 

Containment

B 

EI

q (pressure) 

x

W: deflection in y coordinate 

y

k: Stiffness, Support from Containment

V: projectile velocity 

h 
 3

pressure traveling at the speed of the projectile on the rail can be expressed as a Heaviside step 

function. The governing equation for the rail gun subjected to a moving pressure can then be 

derived as follows: 

kw q[ ] H( ) x Vt . x

w EI

t

w

m + = − − ∂

∂

+

∂

∂ 1 4

4

2

2

 (1) 

Here, w is the lateral displacement, dependent upon time, t, and axial position coordinate, x; m is 

the mass per unit length and is equal to ρΒh; ρ is the density of rail material; and Β and h are the 

width and thickness of the rail, respectively. E is the modulus of rail material, and I is the 

moment of inertia of the rail cross section. The elastic constant, k, due to the elastic foundation, 

will be derived in a later section. The loading function, q[1!H(x !Vt)] in equation (1), represents 

the magnetic pressure front traveling along the rail with a constant velocity, V, represented by a 

Heaviside step function, H(x !Vt). The magnetic pressure, q, is assumed to be constant also. 

Accordingly, 

( ) ( )

 q when x Vt.

q H x Vt when x Vt

= ≤

1− − = 0 >

 (2) 

Equation (1) can be solved using separation of variables with the assumption of 

w(x,t) = φ(t)θ (x). (3) 

Accordingly, the left-hand side of equation (1) can be rewritten to solve the homogeneous 

solution as follows: 

m EI k . '''' φθ + φθ + φθ = 0 && (4) 

The critical velocity of the beam (rail) can be derived from the characteristic function from 

equation (4). The velocity spectrum can be obtained by assuming 

( ) , iN x Vt

w x,t Ae





 



 − = (5) 

where N is wave number and V is the phase velocity. 

Accordingly, the critical velocity can be obtained as follows: 

EI k . B

h Vcr ρ

1

3

2 1 = (6) 

Equation (6) shows that the critical velocity of a railgun subjected to a moving pressure front is a 

function of the rail geometry, density, and elastic modulus. In addition, the support from the 

containment structure has great influence on the dynamic behavior of the rail. Critical velocity 

increases with the elastic modulus of the rails and the stiffness of containment structures. From a 
4

design point of view, a launcher constructed with stiff and lightweight materials is in favor for 

dynamic loading conditions. 

The elastic constant of foundation, k, can be calculated from the containment structure if the 

coupling effects of the insulation material (ceramic in general) are neglected. We consider a 

circular containment of a unit length subjected to concentrated loads at the inner surface of a 

cylinder, as shown in Figure 3(a). Accordingly, the concentrated loads are calculated from the 

summation of resulting magnetic pressure. Because both the containment geometry and loading 

conditions are symmetrical, the structural response can be calculated from the free body shown 

in Figure 3(b). The stiffness of the containment at the location of the concentrated load can then 

be obtained from the strain energy of the curved beam shown in Figure 3(b). Neglecting the 

shear contribution, the strain energy can be expressed as follows: 

d , I E

M R d

A E

N R U

c c

a

c c

θ θ π π= ∫ + ∫

2

0

2 2

0

2

2 2 (7) 

where N is the normal force, Ma is the moment resulting from the concentrated load, and R is the 

mean radius of the containment. Ac, Ic, and Ec are the cross-sectional area, the moment of 

inertia, and elastic modulus of containment, respectively. N and Ma can then be derived as 

follows: 

 , P N cosθ

2 = (8) 

and 

. PR M a 



 



 = −

π

θ 2

cos

2 (9) 

Therefore, the strain energy of the quarter containment can be calculated in terms of 

concentrated load, P, material properties, and geometry. Based on Castigliano’s theorem, the 

displacement at the location of the loading P can then be derived from the derivative of the strain 

energy with respect to the P as follows: 

 , I E

PR

A E

PR

P

U

c c c c

p 



 



 = + − ∂

∂ = 2

3 8 1

16 16 π

π π δ (10) 

where Ic is the bending moment of inertia calculated from a unit length of containment (curved 

beam) shown in Figure 3, which is equal to 3

12

1 bt (b=1). Ec is Young’s modulus of the 

containment. The stiffness constant of the containment can then be defined as 

k P . p= 1 and = 1 δ (11) 
5

Figure 3. Modeling of containment stiffness. 

3. Numerical Results 

A baseline test case is used to obtain critical velocity for a parametric study. The gun is 

composed of a pair of aluminum rails, ceramic insulation, and a steel containment. The 

aluminum rail has a cross section of 12.5 mm (0.5 in) thick × 76.2 mm (3 in) high. The 

containment is 12.5 mm (0.5 in) thick. The parameters required for the simulation are listed in 

Table 1. 

Table 1. Mechanical properties and geometric parameters of the rail and containment. 

Rail (Aluminum) 

Modulus (E) Thickness (h) Height (Β) Density (ρ) 

68.95 GPa 12.5 × 10!3

 m 76.2 × 10!3 m 2750 kg/m3

 

Containment (Steel) 

Modulus (Ec) Thickness (t) Mean Radius (R) 

206.85 GPa 12.5 × 10!3

 m 63.5 × 10!3 m 

The stiffness of the containment can be obtained from equations (10) and (11) by application of 

a unit-concentrated pressure load. The inverse of deflection at the center of the rail (δp) yields 

the stiffness, k, as follows: 

R

N

P/2 Ma

 

O 

Mo

P P

(a) (b)

θ
6

 k = 1 / δp = 3.65 × 109

 Pa . (12) 

The k represents the spring constant of foundation for the entire rail height of 76.2 mm (3.0 in). 

The critical velocity of the barrel can then be calculated from equation (6) as follows: 

 Vcr = 1148 m/s. (13) 

The critical velocity is strongly dependent on the cross-section geometry and the mechanical 

properties of rail and containment. The model is based on the assumption of no structural 

coupling effects from insulation materials. It is a reasonable assumption because the bonding 

between rail and insulation is friction. Parametric studies are performed to compare the baseline 

case that is constructed with aluminum rails and a steel containment, as listed in Table 1. 

Figure 4 shows the effects of rail thickness on the critical velocity of railguns. The geometry of 

containment and all material properties are identical to the baseline case. The increase in the 

moment of inertia of the rail will enhance the bending stiffness of the rail. Accordingly, the 

critical velocity increases with the thickness of the rail. However, the critical velocity does not 

increase linearly; it varies with only a power of 0.25. The stiffness of containment also has 

strong effects on the critical velocity of the railgun. Figure 5 shows the effect of containment 

thickness on the critical velocity of the railgun. A thicker containment provides higher stiffness 

and structural support for the rail. Accordingly, the deflection of containment decreases as it is 

subjected to magnetic pressure from the rails. Mathematically, it is modeled as the stiffness of 

foundation, k, which increases, as illustrated in Figure 5. The effect of the containment stiffness 

on the critical velocity is not linear either; it varies with a power of 0.75. 

Figure 4. Effects of the rail thickness on the critical velocity. 

800

1000

1200

1400

1600

0 10 20 30 40

Rail Thickness (mm)

Critical Velocity (m/sce) ) 
7

Figure 5. Effects of the containment thickness on the critical velocity. 

The effect of rail material properties on the critical velocity is illustrated in Figure 6. A 

combined effect on the dynamic behavior due to the density and elastic modulus of the rail is 

illustrated using some potential material choices. The baseline case is 7075 aluminum alloys. 

Three different conductor materials are examined. GIGAS 24 is an advanced aluminum alloy 

with a higher modulus of 88.25 GPa (12.8 Msi). The density is about the same as the 7075 

aluminum. Accordingly, a higher critical velocity is obtained due to the increase of modulus. 

Figure 6. Effects of the rail material properties on the critical velocity. 

0

500

1000

1500

2000

2500

3000

0 5 10 15 20 25 30 35 40

Containment Thickness (mm)

Critical Velocity (m/sec) ) 

0

200

400

600

800

1000

1200

1400

7075 Al GIGAS24 GlidCop60 Al2O3/Al

Critical Velocity (m/sec)

 Al2O3/Al 

) 
8

Glidcop is aluminum oxide dispersion-strengthened copper. It has a high modulus of 172.4 GPa 

and a high density of 8900 kg/m3

 material. The critical velocity turns out to be lower than the 

7075 aluminum due to the high density. Finally, aluminum reinforced with aluminum oxide 

(Al2O3) fiber (45% volume fraction of fiber content) is used for comparison. The modulus and 

density of this material are 165.5 GPa (24 Msi) and 3400 kg/m3

, respectively. The combination 

of high modulus and low density gives a high-critical velocity. 

4. Conclusions 

The dynamic behavior of an EM barrel can be modeled with reasonable assumptions as a rail 

sitting on an elastic containment. The derived solution illustrates effects of important design 

parameters and material properties on the critical velocity of a barrel, which can be applied for 

barrel design under dynamic conditions. A high magnitude of cyclic stress can occur that might 

cause damage in the rail, accelerate the growth of defect, and eventually shorten the rail life 

significantly. The dynamic phenomenon is particularly crucial if gun barrels are designed to be 

a lightweight and fieldable system with hypervelocity capability. The developed model provides 

a meaningful tool for barrel design that accounts for dynamic response due to a moving 

projectile. 
9

5. References 

1. Taylor, G. I. “Strains in a Gun Barrel Near the Driving Barrel of a Moving Projectile.” 

A.C. 1851/Gn. 104, U.K. Ministry of Supply, London, England, March 1942. 

2. Jones, J. P., and P. G. Bhuta. “Response of Cylindrical Shell to Moving Loads.” Journal of 

Applied Mechanics, vol. 31, Transaction of ASME, vol. 86, Series E, pp. 105–111, March 

1964. 

3. Tang, S. “Dynamic Response of a Tube Under Moving Pressure.” Journal of the 

Engineering Mechanics Division Proceedings of the ASCE, pp. 97–122, October 1965. 

4. Reismann, H. “Response of a Prestressed Cylindrical Shell to Moving Pressure Load, 

Development in Mechanics.” Solid Mechanics – Proceedings of the Eighth Midwestern 

Mechanics Conference, Part II, vol. 2, Pergamon Press, pp. 349–363, 1965. 

5. Simkins, T. E. “Response of Flexural Waves in Gun Tubes.” ARCCB-TR-87008, U.S. 

Army ARDEC, Benet Weapons Laboratory, Watervliet, NY, July 1987. 

6. Hopkins, D. A. “Predicting Dynamic Strain Amplification by Coupling a Finite Element 

Structural Analysis Code With a Gun Interior Ballistic Code.” BRL-TR-3269, U.S. Army 

Ballistic Research Laboratory, Aberdeen Proving Ground, MD, September 1991. 

7. Tzeng, J. T., and D. A. Hopkins. “Dynamic Response of Composite Cylinders Subjected to 

a Moving Internal Pressure.” Journal of Reinforced Plastics and Composites, vol. 15, 

no. 11, pp. 1088–1105, November 1996. 

8. Tzeng, J. T. “Dynamic Fracture of Composite Overwrap Cylinders.” Journal of Reinforced 

Plastics and Composites, vol. 19, no. 1, pp. 2–14, 2000. 

9. Tzeng, J. T. “EM Launcher Structural Design and Material Selection.” IAT-TN-0191, 

Institute of Advanced Technology, The University of Texas at Austin, Austin, TX, July 

2000. 

10. Zielinski, A. “Integrated Launch Package Design With Condition for Reduced Joule 

Demonstration.” ARL-TR-2315, U.S. Army Research Laboratory, Aberdeen Proving 

Ground, MD, January 2001. 
10

INTENTIONALLY LEFT BLANK.
11

radar cross-section modeling, future combat system vehicles, ground vehicle survivability 15

A model is developed to investigate the dynamic response of an electromagnetic rail gun induced by a moving magnetic

pressure during launch of projectiles. As the projectile velocity approaches a critical value, resonance can occur and

cause high-amplitude stress and strain in the rail at the instant and location of the projectile's passage. In this study,

governing equations of a railgun under dynamic-loading conditions are derived that illustrate a lower-bound critical

velocity in terms of material properties, geometry, and barrel cross section. A study is then performed to show the effect

of these parameters on the critical velocity of the barrel. Accordingly, the model that accounts for projectile velocity

and gun construction can be used to guide barrel design.

ARL-TR-2794

U.S. Army Research Laboratory

ATTN: AMSRL-WM-MB

Aberdeen Proving Ground, MD 21005-5069

Jerome T. Tzeng

Critical Velocity of Electromagnetic Rail Gun in Response to Projectile Movement 618622.H80

August 2002 Final, January 2001 - December 2001

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 1 COMMANDER 

 WATERVLIET ARSENAL 

 SMCWV QAE Q 

 B VANINA 

 BLDG 44 

 WATERVLIET NY 12189-4050 

 2 TSM ABRAMS 

 ATZK TS 

 S JABURG 

 W MEINSHAUSEN 

 FT KNOX KY 40121 

 3 ARMOR SCHOOL 

 ATZK TD 

 R BAUEN 

 J BERG 

 A POMEY 

 FT KNOX KY 40121 

 14 COMMANDER 

 US ARMY TACOM 

 AMSTA TR R 

 R MCCLELLAND 

 D THOMAS 

 J BENNETT 

 D HANSEN 

 AMSTA JSK 

 S GOODMAN 

 J FLORENCE 

 K IYER 

 D TEMPLETON 

 A SCHUMACHER 

 AMSTA TR D 

 D OSTBERG 

 L HINOJOSA 

 B RAJU 

 AMSTA CS SF 

 H HUTCHINSON 

 F SCHWARZ 

 WARREN MI 48397-5000 

 15 BENET LABORATORIES 

 AMSTA AR CCB 

 R FISCELLA 

 M SOJA 

 E KATHE 

 P CHEN 

 M SCAVULO 

 G SPENCER 

 P WHEELER 

 S KRUPSKI 

 J VASILAKIS 

 G FRIAR 

 R HASENBEIN 

 AMSTA CCB R 

 S SOPOK 

 E HYLAND 

 D CRAYON 

 R DILLON 

 WATERVLIET NY 12189-4050 

 2 HQ IOC TANK 

 AMMUNITION TEAM 

 AMSIO SMT 

 R CRAWFORD 

 W HARRIS 

 ROCK ISLAND IL 61299-6000 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

6

 2 COMMANDER 

 US ARMY AMCOM 

 AVIATION APPLIED TECH DIR 

 J SCHUCK 

 FT EUSTIS VA 23604-5577 

 1 DIRECTOR 

 US ARMY AMCOM 

 SFAE AV RAM TV 

 D CALDWELL 

 BLDG 5300 

 REDSTONE ARSENAL AL 

 35898 

 2 US ARMY CORPS OF ENGINEERS 

 CERD C 

 T LIU 

 CEW ET 

 T TAN 

 20 MASS AVE NW 

 WASHINGTON DC 20314 

 1 US ARMY COLD REGIONS 

 RSCH & ENGRNG LAB 

 P DUTTA 

 72 LYME RD 

 HANOVER NH 03755 

 1 SYSTEM MANAGER ABRAMS 

 ATZK TS 

 LTC J H NUNN 

 BLDG 1002 RM 110 

 FT KNOX KY 40121 

 1 USA SBCCOM PM SOLDIER SPT 

 AMSSB PM RSS A 

 J CONNORS 

 KANSAS ST 

 NATICK MA 01760-5057 

 2 USA SBCCOM 

 MATERIAL SCIENCE TEAM 

 AMSSB RSS 

 J HERBERT 

 M SENNETT 

 KANSAS ST 

 NATICK MA 01760-5057 

 2 OFC OF NAVAL RESEARCH 

 G GRAF 

 J KELLY 

 800 N QUINCY ST 

 ARLINGTON VA 22217-5660 

 1 NAVAL SURFACE WARFARE CTR 

 DAHLGREN DIV CODE G06 

 DAHLGREN VA 22448 

 1 NAVAL SURFACE WARFARE CTR 

 TECH LIBRARY CODE 323 

 17320 DAHLGREN RD 

 DAHLGREN VA 22448 

 1 NAVAL SURFACE WARFARE CTR 

 CRANE DIVISION 

 M JOHNSON CODE 20H4 

 LOUISVILLE KY 40214-5245 

 8 DIRECTOR 

 US ARMY NATIONAL GROUND 

 INTELLIGENCE CTR 

 D LEITER 

 M HOLTUS 

 M WOLFE 

 S MINGLEDORF 

 J GASTON 

 W GSTATTENBAUER 

 R WARNER 

 J CRIDER 

 220 SEVENTH ST NE 

 CHARLOTTESVILLE VA 22091 

 2 NAVAL SURFACE WARFARE CTR 

 U SORATHIA 

 C WILLIAMS CD 6551 

 9500 MACARTHUR BLVD 

 WEST BETHESDA MD 20817 

 2 COMMANDER 

 NAVAL SURFACE WARFARE CTR 

 CARDEROCK DIVISION 

 R PETERSON CODE 2020 

 M CRITCHFIELD CODE 1730 

 BETHESDA MD 20084 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

7

 8 US ARMY SBCCOM 

 SOLDIER SYSTEMS CENTER 

 BALLISTICS TEAM 

 J WARD 

 W ZUKAS 

 P CUNNIFF 

 J SONG 

 MARINE CORPS TEAM 

 J MACKIEWICZ 

 BUS AREA ADVOCACY TEAM 

 W HASKELL 

 AMSSB RCP SS 

 W NYKVIST 

 S BEAUDOIN 

 KANSAS ST 

 NATICK MA 01760-5019 

 12 US ARMY RESEARCH OFC 

 A CROWSON 

 J CHANDRA 

 H EVERETT 

 J PRATER 

 R SINGLETON 

 G ANDERSON 

 D STEPP 

 D KISEROW 

 J CHANG 

 M ZIKERY 

 J WU 

 B LAMATTINA 

 PO BOX 12211 

 RESEARCH TRIANGLE PARK NC 

 27709-2211 

 8 NAVAL SURFACE WARFARE CTR 

 J FRANCIS CODE G30 

 D WILSON CODE G32 

 R D COOPER CODE G32 

 J FRAYSSE CODE G33 

 E ROWE CODE G33 

 T DURAN CODE G33 

 L DE SIMONE CODE G33 

 R HUBBARD CODE G33 

 DAHLGREN VA 22448 

 1 NAVAL SEA SYSTEMS CMD 

 D LIESE 

 2531 JEFFERSON DAVIS HWY 

 ARLINGTON VA 22242-5160 

 1 NAVAL SURFACE WARFARE CTR 

 M LACY CODE B02 

 17320 DAHLGREN RD 

 DAHLGREN VA 22448 

 2 NAVAL SURFACE WARFARE CTR 

 CARDEROCK DIVISION 

 R CRANE CODE 2802 

 C WILLIAMS CODE 6553 

 3A LEGGETT CIR 

 BETHESDA MD 20054-5000 

 1 EXPEDITIONARY WARFARE 

 DIV N85 

 F SHOUP 

 2000 NAVY PENTAGON 

 WASHINGTON DC 20350-2000 

 1 AFRL MLBC 

 2941 P ST RM 136 

 WRIGHT PATTERSON AFB OH 

 45433-7750 

 1 AFRL MLSS 

 R THOMSON 

 2179 12TH ST RM 122 

 WRIGHT PATTERSON AFB OH 

 45433-7718 

 2 AFRL 

 F ABRAMS 

 J BROWN 

 BLDG 653 

 2977 P ST STE 6 

 WRIGHT PATTERSON AFB OH 

 45433-7739 

 1 WATERWAYS EXPERIMENT 

 D SCOTT 

 3909 HALLS FERRY RD SC C 

 VICKSBURG MS 39180 

 5 DIRECTOR 

 LLNL 

 R CHRISTENSEN 

 S DETERESA 

 F MAGNESS 

 M FINGER MS 313 

 M MURPHY L 282 

 PO BOX 808 

 LIVERMORE CA 94550 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

8

 1 AFRL MLS OL 

 L COULTER 

 7278 4TH ST 

 BLDG 100 BAY D 

 HILL AFB UT 84056-5205 

 1 OSD 

 JOINT CCD TEST FORCE 

 OSD JCCD 

 R WILLIAMS 

 3909 HALLS FERRY RD 

 VICKSBURG MS 29180-6199 

 1 DEFENSE NUCLEAR AGENCY 

 INNOVATIVE CONCEPTS DIV 

 6801 TELEGRAPH RD 

 ALEXANDRIA VA 22310-3398 

 6 DARPA 

 M VANFOSSEN 

 S WAX 

 L CHRISTODOULOU 

 B WILCOX 

 M FREEMAN 

 S FISH 

 3701 N FAIRFAX DR 

 ARLINGTON VA 22203-1714 

 2 SERDP PROGRAM OFC 

 PM P2 

 C PELLERIN 

 B SMITH 

 901 N STUART ST STE 303 

 ARLINGTON VA 22203 

 1 FAA 

 MIL HDBK 17 CHAIR 

 L ILCEWICZ 

 1601 LIND AVE SW 

 ANM 115N 

 RESTON VA 98055 

 1 US DEPT OF ENERGY 

 OFC OF ENVIRONMENTAL 

 MANAGEMENT 

 P RITZCOVAN 

 19901 GERMANTOWN RD 

 GERMANTOWN MD 20874-1928 

 1 DIRECTOR 

 LLNL 

 F ADDESSIO MS B216 

 PO BOX 1633 

 LOS ALAMOS NM 87545 

 1 OAK RIDGE NATIONAL 

 LABORATORY 

 R M DAVIS 

 PO BOX 2008 

 OAK RIDGE TN 37831-6195 

 3 DIRECTOR 

 SANDIA NATIONAL LABS 

 APPLIED MECHANICS DEPT 

 MS 9042 

 J HANDROCK 

 Y R KAN 

 J LAUFFER 

 PO BOX 969 

 LIVERMORE CA 94551-0969 

 1 OAK RIDGE NATIONAL 

 LABORATORY 

 C EBERLE MS 8048 

 PO BOX 2008 

 OAK RIDGE TN 37831 

 1 OAK RIDGE NATIONAL 

 LABORATORY 

 C D WARREN MS 8039 

 PO BOX 2008 

 OAK RIDGE TN 37831 

 5 NIST 

 J DUNKERS 

 M VANLANDINGHAM MS 8621 

 J CHIN MS 8621 

 J MARTIN MS 8621 

 D DUTHINH MS 8611 

 100 BUREAU DR 

 GAITHERSBURG MD 20899 

 1 HYDROGEOLOGIC INC 

 SERDP ESTCP SPT OFC 

 S WALSH 

 1155 HERNDON PKWY STE 900 

 HERNDON VA 20170 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

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 4 NASA LANGLEY RSCH CTR 

 AMSRL VS 

 W ELBER MS 266 

 F BARTLETT JR MS 266 

 G FARLEY MS 266 

 T K OBRIEN 

 HAMPTON VA 23681-0001 

 1 NASA LANGLEY RSCH CTR 

 T GATES MS 188E 

 HAMPTON VA 23661-3400 

 1 FHWA 

 E MUNLEY 

 6300 GEORGETOWN PIKE 

 MCLEAN VA 22101 

 3 CYTEC FIBERITE 

 R DUNNE 

 D KOHLI 

 R MAYHEW 

 1300 REVOLUTION ST 

 HAVRE DE GRACE MD 21078 

 1 USDOT FEDERAL RAILRD 

 M FATEH RDV 31 

 WASHINGTON DC 20590 

 1 MARINE CORPS 

 INTLLGNC ACTVTY 

 D KOSITZKE 

 3300 RUSSELL RD STE 250 

 QUANTICO VA 22134-5011 

 1 DIRECTOR 

 NATIONAL GRND INTLLGNC CTR 

 IANG TMT 

 220 SEVENTH ST NE 

 CHARLOTTESVILLE VA 

 22902-5396 

 1 SIOUX MFG 

 B KRIEL 

 PO BOX 400 

 FT TOTTEN ND 58335 

 2 3TEX CORPORATION 

 A BOGDANOVICH 

 J SINGLETARY 

 109 MACKENAN DR 

 CARY NC 27511 

 1 3M CORPORATION 

 J SKILDUM 

 3M CENTER BLDG 60 IN 01 

 ST PAUL MN 55144-1000 

 1 DIRECTOR 

 DEFENSE INTLLGNC AGNCY 

 TA 5 

 K CRELLING 

 WASHINGTON DC 20310 

 1 ADVANCED GLASS FIBER YARNS 

 T COLLINS 

 281 SPRING RUN LANE STE A 

 DOWNINGTON PA 19335 

 1 COMPOSITE MATERIALS INC 

 D SHORTT 

 19105 63 AVE NE 

 PO BOX 25 

 ARLINGTON WA 98223 

 1 JPS GLASS 

 L CARTER 

 PO BOX 260 

 SLATER RD 

 SLATER SC 29683 

 1 COMPOSITE MATERIALS INC 

 R HOLLAND 

 11 JEWEL CT 

 ORINDA CA 94563 

 1 COMPOSITE MATERIALS INC 

 C RILEY 

 14530 S ANSON AVE 

 SANTA FE SPRINGS CA 90670 

 2 SIMULA 

 J COLTMAN 

 R HUYETT 

 10016 S 51ST ST 

 PHOENIX AZ 85044 

 2 PROTECTION MATERIALS INC 

 M MILLER 

 F CRILLEY 

 14000 NW 58 CT 

 MIAMI LAKES FL 33014 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

10

 2 FOSTER MILLER 

 M ROYLANCE 

 W ZUKAS 

 195 BEAR HILL RD 

 WALTHAM MA 02354-1196 

 1 ROM DEVELOPMENT CORP 

 R O MEARA 

 136 SWINEBURNE ROW 

 BRICK MARKET PLACE 

 NEWPORT RI 02840 

 2 TEXTRON SYSTEMS 

 T FOLTZ 

 M TREASURE 

 1449 MIDDLESEX ST 

 LOWELL MA 01851 

 1 O GARA HESS & EISENHARDT 

 M GILLESPIE 

 9113 LESAINT DR 

 FAIRFIELD OH 45014 

 2 MILLIKEN RSCH CORP 

 H KUHN 

 M MACLEOD 

 PO BOX 1926 

 SPARTANBURG SC 29303 

 1 CONNEAUGHT INDUSTRIES INC 

 J SANTOS 

 PO BOX 1425 

 COVENTRY RI 02816 

 1 BATTELLE NATICK OPNS 

 B HALPIN 

 209 W CENTRAL ST STE 302 

 NATICK MA 01760 

 1 ARMTEC DEFENSE PRODUCTS 

 S DYER 

 85 901 AVE 53 

 PO BOX 848 

 COACHELLA CA 92236 

 1 NATIONAL COMPOSITE CENTER 

 T CORDELL 

 2000 COMPOSITE DR 

 KETTERING OH 45420 

 3 PACIFIC NORTHWEST LAB 

 M SMITH 

 G VAN ARSDALE 

 R SHIPPELL 

 PO BOX 999 

 RICHLAND WA 99352 

 2 AMOCO PERFORMANCE 

 PRODUCTS 

 M MICHNO JR 

 J BANISAUKAS 

 4500 MCGINNIS FERRY RD 

 ALPHARETTA GA 30202-3944 

 8 ALLIANT TECHSYSTEMS INC 

 C CANDLAND MN11 2830 

 C AAKHUS MN11 2830 

 B SEE MN11 2439 

 N VLAHAKUS MN11 2145 

 R DOHRN MN11 2830 

 S HAGLUND MN11 2439 

 M HISSONG MN11 2830 

 D KAMDAR MN11 2830 

 600 SECOND ST NE 

 HOPKINS MN 55343-8367 

 3 SAIC 

 M PALMER 

 A WALLS 

 W REINSTRA 

 1410 SPRING HILL RD STE 400 

 MS SH4 5 

 MCLEAN VA 22102 

 1 SAIC 

 G CHRYSSOMALLIS 

 3800 W 80TH ST STE 1090 

 BLOOMINGTON MN 55431 

 1 AAI CORPORATION 

 T G STASTNY 

 PO BOX 126 

 HUNT VALLEY MD 21030-0126 

 1 APPLIED COMPOSITES 

 W GRISCH 

 333 NORTH SIXTH ST 

 ST CHARLES IL 60174 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

11

 1 CUSTOM ANALYTICAL 

 ENG SYS INC 

 A ALEXANDER 

 13000 TENSOR LANE NE 

 FLINTSTONE MD 21530 

 3 ALLIANT TECHSYSTEMS INC 

 J CONDON 

 E LYNAM 

 J GERHARD 

 WV01 16 STATE RT 956 

 PO BOX 210 

 ROCKET CENTER WV 26726-0210 

 1 OFC DEPUTY UNDER SEC DEFNS 

 J THOMPSON 

 1745 JEFFERSON DAVIS HWY 

 CRYSTAL SQ 4 STE 501 

 ARLINGTON VA 22202 

 1 PROJECTILE TECHNOLOGY INC 

 515 GILES ST 

 HAVRE DE GRACE MD 21078 

 5 AEROJET GEN CORP 

 D PILLASCH 

 T COULTER 

 C FLYNN 

 D RUBAREZUL 

 M GREINER 

 1100 WEST HOLLYVALE ST 

 AZUSA CA 91702-0296 

 3 HEXCEL INC 

 R BOE 

 PO BOX 18748 

 SALT LAKE CITY UT 84118 

 1 HERCULES INC 

 HERCULES PLAZA 

 WILMINGTON DE 19894 

 1 BRIGS COMPANY 

 J BACKOFEN 

 2668 PETERBOROUGH ST 

 HERNDON VA 22071-2443 

 1 ZERNOW TECHNICAL SERVICES 

 L ZERNOW 

 425 W BONITA AVE STE 208 

 SAN DIMAS CA 91773 

 1 GENERAL DYNAMICS OTS 

 L WHITMORE 

 10101 NINTH ST NORTH 

 ST PETERSBURG FL 33702 

 3 GENERAL DYNAMICS OTS 

 FLINCHBAUGH DIV 

 E STEINER 

 B STEWART 

 T LYNCH 

 PO BOX 127 

 RED LION PA 17356 

 1 GKN AEROSPACE 

 D OLDS 

 15 STERLING DR 

 WALLINGFORD CT 06492 

 5 SIKORSKY AIRCRAFT 

 G JACARUSO 

 T CARSTENSAN 

 B KAY 

 S GARBO MS S330A 

 J ADELMANN 

 6900 MAIN ST 

 PO BOX 9729 

 STRATFORD CT 06497-9729 

 1 PRATT & WHITNEY 

 C WATSON 

 400 MAIN ST MS 114 37 

 EAST HARTFORD CT 06108 

 1 AEROSPACE CORP 

 G HAWKINS M4 945 

 2350 E EL SEGUNDO BLVD 

 EL SEGUNDO CA 90245 

 2 CYTEC FIBERITE 

 M LIN 

 W WEB 

 1440 N KRAEMER BLVD 

 ANAHEIM CA 92806 

 1 UDLP 

 G THOMAS 

 PO BOX 58123 

 SANTA CLARA CA 95052 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

12

 2 UDLP 

 R BARRETT MAIL DROP M53 

 V HORVATICH MAIL DROP M53 

 328 W BROKAW RD 

 SANTA CLARA CA 95052-0359 

 3 UDLP 

 GROUND SYSTEMS DIVISION 

 M PEDRAZZI MAIL DROP N09 

 A LEE MAIL DROP N11 

 M MACLEAN MAIL DROP N06 

 1205 COLEMAN AVE 

 SANTA CLARA CA 95052 

 4 UDLP 

 R BRYNSVOLD 

 P JANKE MS 170 

 4800 EAST RIVER RD 

 MINNEAPOLIS MN 55421-1498 

 1 UDLP 

 D MARTIN 

 PO BOX 359 

 SANTA CLARA CA 95052 

 2 BOEING DFNSE & SPACE GP 

 W HAMMOND S 4X55 

 J RUSSELL S 4X55 

 PO BOX 3707 

 SEATTLE WA 98124-2207 

 2 BOEING ROTORCRAFT 

 P MINGURT 

 P HANDEL 

 800 B PUTNAM BLVD 

 WALLINGFORD PA 19086 

 1 BOEING 

 DOUGLAS PRODUCTS DIV 

 L J HART SMITH 

 3855 LAKEWOOD BLVD 

 D800 0019 

 LONG BEACH CA 90846-0001 

 1 LOCKHEED MARTIN 

 SKUNK WORKS 

 D FORTNEY 

 1011 LOCKHEED WAY 

 PALMDALE CA 93599-2502 

 1 LOCKHEED MARTIN 

 R FIELDS 

 1195 IRWIN CT 

 WINTER SPRINGS FL 32708 

 1 MATERIALS SCIENCES CORP 

 G FLANAGAN 

 500 OFC CENTER DR STE 250 

 FT WASHINGTON PA 19034 

 1 NORTHRUP GRUMMAN CORP 

 ELECTRONIC SENSORS 

 & SYSTEMS DIV 

 E SCHOCH MS V 16 

 1745A W NURSERY RD 

 LINTHICUM MD 21090 

 1 GDLS DIVISION 

 D BARTLE 

 PO BOX 1901 

 WARREN MI 48090 

 2 GDLS 

 D REES 

 M PASIK 

 PO BOX 2074 

 WARREN MI 48090-2074 

 1 GDLS 

 MUSKEGON OPERATIONS 

 W SOMMERS JR 

 76 GETTY ST 

 MUSKEGON MI 49442 

 1 GENERAL DYNAMICS 

 AMPHIBIOUS SYS 

 SURVIVABILITY LEAD 

 G WALKER 

 991 ANNAPOLIS WAY 

 WOODBRIDGE VA 22191 

 8 INST FOR ADVANCED 

 TECH 

 H FAIR 

 I MCNAB 

 P SULLIVAN 

 S BLESS 

 W REINECKE 

 C PERSAD 

 M CRAWFORD 

 K T HSIEH 

 3925 W BRAKER LN STE 400 

 AUSTIN TX 78759-5316 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

13

 2 CIVIL ENGR RSCH FOUNDATION 

 PRESIDENT 

 H BERNSTEIN 

 R BELLE 

 1015 15TH ST NW STE 600 

 WASHINGTON DC 20005 

 1 ARROW TECH ASSO 

 1233 SHELBURNE RD STE D8 

 SOUTH BURLINGTON VT 

 05403-7700 

 1 R EICHELBERGER 

 CONSULTANT 

 409 W CATHERINE ST 

 BEL AIR MD 21014-3613 

 1 UCLA MANE DEPT ENGR IV 

 H T HAHN 

 LOS ANGELES CA 90024-1597 

 2 UNIV OF DAYTON 

 RESEARCH INST 

 R Y KIM 

 A K ROY 

 300 COLLEGE PARK AVE 

 DAYTON OH 45469-0168 

 1 UMASS LOWELL 

 PLASTICS DEPT 

 N SCHOTT 

 1 UNIVERSITY AVE 

 LOWELL MA 01854 

 1 IIT RESEARCH CENTER 

 D ROSE 

 201 MILL ST 

 ROME NY 13440-6916 

 1 GA TECH RSCH INST 

 GA INST OF TCHNLGY 

 P FRIEDERICH 

 ATLANTA GA 30392 

 1 MICHIGAN ST UNIV 

 MSM DEPT 

 R AVERILL 

 3515 EB 

 EAST LANSING MI 48824-1226 

 1 UNIV OF WYOMING 

 D ADAMS 

 PO BOX 3295 

 LARAMIE WY 82071 

 2 PENN STATE UNIV 

 R MCNITT 

 C BAKIS 

 212 EARTH ENGR 

 SCIENCES BLDG 

 UNIVERSITY PARK PA 16802 

 1 PENN STATE UNIV 

 R S ENGEL 

 245 HAMMOND BLDG 

 UNIVERSITY PARK PA 16801 

 1 PURDUE UNIV 

 SCHOOL OF AERO & ASTRO 

 C T SUN 

 W LAFAYETTE IN 47907-1282 

 1 STANFORD UNIV 

 DEPT OF AERONAUTICS 

 & AEROBALLISTICS 

 S TSAI 

 DURANT BLDG 

 STANFORD CA 94305 

 1 UNIV OF MAINE 

 ADV STR & COMP LAB 

 R LOPEZ ANIDO 

 5793 AEWC BLDG 

 ORONO ME 04469-5793 

 1 JOHNS HOPKINS UNIV 

 APPLIED PHYSICS LAB 

 P WIENHOLD 

 11100 JOHNS HOPKINS RD 

 LAUREL MD 20723-6099 

 1 UNIV OF DAYTON 

 J M WHITNEY 

 COLLEGE PARK AVE 

 DAYTON OH 45469-0240 

 1 DEPT OF MATERIALS 

 SCIENCE & ENGINEERING 

 UNIVERSITY OF ILLINOIS 

 AT URBANA CHAMPAIGN 

 J ECONOMY 

 1304 WEST GREEN ST 115B 

 URBANA IL 61801 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

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 5 UNIV OF DELAWARE 

 CTR FOR COMPOSITE MTRLS 

 J GILLESPIE 

 M SANTARE 

 S YARLAGADDA 

 S ADVANI 

 D HEIDER 

 201 SPENCER LABORATORY 

 NEWARK DE 19716 

 1 NORTH CAROLINA STATE UNIV 

 CIVIL ENGINEERING DEPT 

 W RASDORF 

 PO BOX 7908 

 RALEIGH NC 27696-7908 

 1 UNIV OF MARYLAND 

 DEPT OF AEROSPACE ENGNRNG 

 A J VIZZINI 

 COLLEGE PARK MD 20742 

 4 UNIV OF TEXAS AT AUSTIN 

 CTR FOR ELECTROMECHANICS 

 M WERST 

 J HAHNE 

 R THOMPSON 

 J KITZMILLER 

 10100 BURNET RD 

 AUSTIN TX 78758-4497 

 4 VA POLYTECHNICAL 

 INST & STATE UNIV 

 DEPT OF ESM 

 M W HYER 

 K REIFSNIDER 

 S CASE 

 A LOOS 

 BLACKSBURG VA 24061-0219 

 2 DREXEL UNIV 

 A S D WANG 

 W SUN 

 32ND & CHESTNUT ST 

 PHILADELPHIA PA 19104 

 1 SOUTHWEST RSCH INST 

 ENGR & MATL SCIENCES DIV 

 J RIEGEL 

 6220 CULEBRA RD 

 PO DRAWER 28510 

 SAN ANTONIO TX 78228-0510 

 1 COMMANDER 

 US ARMY TACOM ARDEC 

 AMSTA AR FSP 

 D LADD 

 BLDG 354 

 PICATINNY ARSENAL NJ 

 07806-5000 

 4 LOCKHEED MARTIN VOUGHT 

 L FARRIS 

 T HOU 

 N WELLS 

 K COOKS 

 PO BOX 650003 

 MS WT 21 

 DALLAS TX 75625-0003 

 1 UNIV AT BUFFALO SUNY AB 

 J SARJEANT 

 PO BOX 601900 

 BUFFALO NY 14260-1900 

 1 KAMAN ELECTROMAGNETICS 

 CORP 

 P MONGEAU 

 2 FOX RD 

 HUDSON MA 01749 

 1 SAIC 

 B RIENSTRA 

 8200 N MOPAC EXPRESSWAY 

 SUITE 150 

 AUSTIN TX 78759 

 1 SAIC 

 K A JAMISON 

 1247 B N EGLIN PKWY 

 SHALIMAR FL 32579 

 2 IAP RESEARCH INC 

 D BAUER 

 J BARBER 

 2763 CULVER AVE 

 DAYTON OH 45429-3723 

 3 MAXWELL TECHNOLOGIES 

 P REIDY 

 T WOLFE 

 9244 BALBOA AVENUE 

 SAN DIEGO CA 92123 
NO. OF NO. OF 

COPIES ORGANIZATION COPIES ORGANIZATION

15

 1 MAXWELL PHYSICS 

 INTERNATIONAL 

 C GILMAN 

 2700 MERCED STREET 

 PO BOX 5010 

 SAN LEANDRO CA 94577-0599 

ABERDEEN PROVING GROUND 

 1 US ARMY MATERIEL 

 SYSTEMS ANALYSIS ACTIVITY 

 P DIETZ 

 392 HOPKINS RD 

 AMXSY TD 

 APG MD 21005-5071 

 1 DIRECTOR 

 US ARMY RESEARCH LAB 

 AMSRL OP AP L 

 APG MD 21005-5066 

 93 DIR USARL 

 AMSRL CI 

 AMSRL CI H 

 W STUREK 

 AMSRL CI S 

 A MARK 

 AMSRL CS IO FI 

 M ADAMSON 

 AMSRL SL BA 

 AMSRL SL BL 

 D BELY 

 R HENRY 

 AMSRL SL BG 

 AMSRL SL I 

 AMSRL WM 

 J SMITH 

 AMSRL WM B 

 E SCHMIDT 

 A HORST 

 AMSRL WM BA 

 D LYON 

 AMSRL WM BC 

 P PLOSTINS 

 J NEWILL 

 S WILKERSON 

 A ZIELINSKI 

ABERDEEN PROVING GROUND (CONT)

 AMSRL WM BD 

 B FORCH 

 R FIFER 

 R PESCE RODRIGUEZ 

 B RICE 

 AMSRL WM BE 

 C LEVERITT 

 AMSRL WM BF 

 J LACETERA 

 AMSRL WM BR 

 C SHOEMAKER 

 J BORNSTEIN 

 AMSRL WM M 

 D VIECHNICKI 

 G HAGNAUER 

 J MCCAULEY 

 AMSRL WM MA 

 L GHIORSE 

 S MCKNIGHT 

 AMSRL WM MB 

 B FINK 

 J BENDER 

 T BOGETTI 

 R BOSSOLI 

 L BURTON 

 K BOYD 

 S CORNELISON 

 P DEHMER 

 R DOOLEY 

 W DRYSDALE 

 G GAZONAS 

 S GHIORSE 

 D GRANVILLE 

 D HOPKINS 

 C HOPPEL 

 D HENRY 

 R KASTE 

 M KLUSEWITZ 

 M LEADORE 

 R LIEB 

 E RIGAS 

 J SANDS 

 D SPAGNUOLO 

 W SPURGEON 

 J TZENG 

 E WETZEL 

 A FRYDMAN 
NO. OF 

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ABERDEEN PROVING GROUND (CONT)

 AMRSL WM MC 

 J BEATTY 

 E CHIN 

 J MONTGOMERY 

 A WERECZCAK 

 J LASALVIA 

 J WELLS 

 AMSRL WM MD 

 W ROY 

 S WALSH 

 AMSRL WM T 

 T WRIGHT 

 B BURNS 

 M ZOLTOSKI 

 AMSRL WM TA 

 W GILLICH 

 T HAVEL 

 J RUNYEON 

 M BURKINS 

 E HORWATH 

 B GOOCH 

 W BRUCHEY 

 M NORMANDIA 

 AMRSL WM TB 

 D KOOKER 

 P BAKER 

 AMSRL WM TC 

 R COATES 

 AMSRL WM TD 

 A DAS GUPTA 

 T HADUCH 

 T MOYNIHAN 

 F GREGORY 

 M RAFTENBERG 

 M BOTELER 

 T WEERASOORIYA 

 D DANDEKAR 

 A DIETRICH 

 AMSRL WM TE 

 A NIILER 

 J POWELL 

 AMSRL SS SD 

 H WALLACE 

 AMSRL SS SE DS 

 R REYZER 

 R ATKINSON 
NO. OF NO. OF 

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 1 LTD 

 R MARTIN 

 MERL 

 TAMWORTH RD 

 HERTFORD SG13 7DG 

 UK 

 1 SMC SCOTLAND 

 P W LAY 

 DERA ROSYTH 

 ROSYTH ROYAL DOCKYARD 

 DUNFERMLINE FIFE KY 11 2XR 

 UK 

 1 CIVIL AVIATION 

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 T GOTTESMAN 

 PO BOX 8 

 BEN GURION INTERNL AIRPORT 

 LOD 70150 

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 1 AEROSPATIALE 

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 A BTE CC RTE MD132 

 316 ROUTE DE BAYONNE 

 TOULOUSE 31060 

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 P N JONES 

 SEVEN OAKS KENT TN 147BP 

 UK 

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 F LESAGE 

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 3602 THUN 

 SWITZERLAND 

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 HAIFA 3200 

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 1 DSTO 

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 N BURMAN RLLWS 

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 SOUTH AUSTRALIA 5108 

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 1040 BRUXELLE 

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 2459 BOULEVARD PIE XI NORTH 

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 CANADA 

 PO BOX 8800 COURCELETTE 

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 CANADA 

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 J MANSON 

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 CH 1015 LAUSANNE 

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NO. OF 

COPIES ORGANIZATION 

18

 1 TNO PRINS MAURITS 

 LABORATORY 

 R IJSSELSTEIN 

 LANGE KLEIWEG 137 

 PO BOX 45 

 2280 AA RIJSWIJK 

 THE NETHERLANDS 

 2 FOA NATL DEFENSE RESEARCH 

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 DIR DEPT OF WEAPONS & 

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 B JANZON 

 R HOLMLIN 

 S 172 90 STOCKHOLM 

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 GROUND 

 I CREWTHER 

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 3602 THUN 

 SWITZERLAND 

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 M MAYSELESS 

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 HAIFA 31021 

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 D 86523 SCHROBENHAUSEN 

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