Problems associated with launching hypervelocity projectiles from the Fast Shock Tube
Modeling and experiments are being done with the goal of understanding the physics of projectile acceleration at high driving pressures (megabar range) and short acceleration times (a few microseconds) well enough to design and test successful hypervelocity launch systems. The Fast Shock Tube, a cylindrically convergent high-explosive driver, has been used to accelerate projectiles. Detailed modeling of the experiments, including high-pressure gas flow, projectile instability, and projectile fracture, has been done with MESA/2D. Modeling results show quantitative agreement with the average behavior of the system. However, details of projectile behavior are not predicted well. Observed velocity distributions across the diameter of a projectile or projectile shapes are only in qualitative agreement with calculations. This, then, presents the major constraint on the successful design of a launch system: that the processes that limit projectile integrity depend on the details of the drive conditions, and these details are not quantitatively modeled at this time.
- Research Organization:
- Los Alamos National Laboratory (LANL), Los Alamos, NM (United States)
- Sponsoring Organization:
- USDOE; USDOE, Washington, DC (United States)
- DOE Contract Number:
- W-7405-ENG-36
- OSTI ID:
- 5095128
- Report Number(s):
- LA-UR-92-1529; ON: DE92015276
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
42 ENGINEERING
PROJECTILES
ACCELERATION
SHOCK TUBES
PERFORMANCE
DENSITY
FOAMS
GASES
MATHEMATICAL MODELS
STABILITY
VELOCITY
COLLOIDS
DISPERSIONS
FLUIDS
PHYSICAL PROPERTIES
450000* - Military Technology
Weaponry
& National Defense
420500 - Engineering- Materials Testing