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Some Comments Regarding Performance Potential for a New Machine Gun and Ammunition Concepts Abe Flatau Consultant.

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Presentation on theme: "Some Comments Regarding Performance Potential for a New Machine Gun and Ammunition Concepts Abe Flatau Consultant."— Presentation transcript:

1 Some Comments Regarding Performance Potential for a New Machine Gun and Ammunition Concepts
Abe Flatau Consultant

2 General Outline Summary Introduction Brief Technical Overview
Ammunition Emphasis on lightweight, high V0, very low drag projectiles = high kinetic energy to deposit on target Brief Comparison of Trajectory Profiles Proposed vs. current

3 Conclusion It is strongly recommended that the key technologies be brought together to result in a modern, high performance, effective machine gun system that is a superior weapon in the field.

4 Summary Conceiving, developing and fielding a weapon system is not an easy task. Perhaps that is why we shy away from replacing tried and tested systems that have been used for almost the past century. This brief presentation points out some of the advances in technology that can be applied to a new high performance machine gun system.

5 Comments on .50 Cal Heavy Machine Gun
Technology from the end of WWI (1918). Cartridge volume is limited. No significant increase in performance. Saboted Light Anti-Material Penetrator (SLAP) performance limited. Overall gun-ammo system limited for performance upgrade.

6 Aerodynamicist’s Golden Rule
“Assume Everything, But the Responsibility.”

7 Current and Proposed Heavy Machine Gun Systems
Wt (lb) V0(ft/sec) US mm(.50cal) ,800 US mm(.60cal) US mm(.65cal) ,000 Soviet mm(.57cal) ,511 US mm M ,380

8 Characteristics of Well Designed Tubular Projectiles
High muzzle velocity +Low drag shape = High kinetic energy + short time of flight = relatively flat trajectory = high hit probability Performance bonus = high gyroscopic stability = anti-ricochet

9 Relatively New Technologies (Since Browning .50 Cal was Accepted)
Aeroballistic Interior Ballistics Materials (high strength & light weight) Computer Aided Design

10 Projectiles Tubular w/ Incendiary Pusher/obturator Multipurpose
Consumable Conventional w/ HE Charge SLAP

11 Interior Ballistics Compacted propellant
(Proprietary designs and concepts) Ignition Techniques Lightweight projectile Mass (M) + High muzzle velocity (V) = High kinetic energy (1/2MV2) Equates to: Shorter time of flight to a given distance + some aerodynamic lift combined with low-aerodynamic drag = a relatively flat trajectory

12 Packing Density WWII Propeller Aircraft Jet Fighter

13 Conclusion It is strongly recommended that the key technologies be brought together to result in a modern, high performance, effective machine gun and ammunition system that is superior to other gun-launched weapons in its general class.

14 Full-bore Tubular Projectile Configuration
Air flow Lip angle Rotating band Crimp groove Boattail Convergent area Throat Divergent area

15 Basic Characteristics of Tubular Projectiles
Flight direction Low supersonic drag Light weight allows increased muzzle velocity High gyroscope stability

16 External Flow Characteristics of Tubular Projectiles
High Mach Number Low Mach Number M  1.9 Direction of flight Swallowed flow No bow shock on or in front of nose Low drag Choked flow Bow shock High drag

17 Bow shock associated with “choking” and high drag
Note: Above shape is known as a Busemann Biplane and also as an “internal” design

18 Before high drag condition
Schlieren Photographs of TCD-3 WSCO Supersonic Wind Tunnel Variable Mach Number Operation M  3.0 M  2.5 M  1.6 M  2.0 Before high drag condition High drag condition

19 Aeroballistic Range Photographs/TCD-3
M ~ 40 Near muzzle 20 feet down range 15 feet down range 300 feet down range

20 Tubular projectile M103 case
Obturator/ pusher M103 case WSC MAR 76

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22 Potential Advantages of Tubular Projectiles
Higher launch velocity (lighter weight) Shorter time of flight Near straight-line trajectory profile Simplified fire control

23 Kinetic Energy vs. Range
500 1000 1500 2000 Range, meters 40 30 25 20 15 10 5 Kinetic energy, ft-lb  103 0.5 sec 1.0 1.5 2.0 2.5 3.0 3.5 4.0 Size Weight, lb Vo, ft/sec 0.65 cal 14.5 mm api 0.50 cal. apm 20 mm M

24 T-0.65 Caliber vs. 0.50 Caliber Caliber Weight, lb T-0.65 0.0794
5000 4000 3000 2000 1000 Velocity, ~ft/sec Range, ~meters 0.5 sec 1.0 1.5 2.0 2.5 3.0 4.0 0.7 sec 2.8

25 Representative Trajectory Profiles
.50 cal. AP:  = 2, V0 = 2800 FPS .60 cal. TCD-7:  = 0.6, V0 = 5000 FPS 500 1000 1500 2000 40 30 20 10 Horizontal range, ~meters Height, meters Vi.65 cal = 1028 FPS t = 2.60 sec and Vi.50 cal = 815 FPS t = 4.50 sec

26 Summary of .65 Caliber Tubular Projectile Characteristics
Significant increase in kinetic energy over .50 caliber Terminal ballistics far superior to .50 caliber AP Flatter trajectory than .50 caliber Shorter time of flight than .50 caliber Greater range than .50 caliber Low weight system/low cost ammunition DRDAR-ACW

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28 “That’s how Research and Development put the pressure on
“That’s how Research and Development put the pressure on. First they hustle you to promise them results. Then they hustle you some more to promise them results in our lifetime!”


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