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Quantitative Effects of Projectile-Launch Tube Wall Friction on Ballistic Range Operation

Authors :
Shinji Ohba
Akihiro Sasoh
Kazuyoshi Takayama
Source :
AIAA Journal. 38:1709-1715
Publication Year :
2000
Publisher :
American Institute of Aeronautics and Astronautics (AIAA), 2000.

Abstract

Theoretical and experimental studies are conducted on the quantitative evaluation of a friction force at the interface between a projectile and the launch tube wall in a ballistic range. From a mechanical balance relation applied to the projectile, the friction force is expressed theoretically as a function of the net acceleration of the projectile. With this formulation, experimentally measured in-bore projectile velocity proe les obtained using a velocity interferometer system for any ree ector are well interpreted. If the initial projectile motion is signie cantly suppressed by the friction force while the burning rate of the propellant remains signie cant, the base pressure becomes much higher than that with a negligibly small friction force, thereby enhancing the net acceleration. However, if the projectile-tube e t is excessively high, the main function of the friction force is to decrease the muzzle velocity.

Details

ISSN :
1533385X and 00011452
Volume :
38
Database :
OpenAIRE
Journal :
AIAA Journal
Accession number :
edsair.doi...........a3c305128a8dc40295836af12a9179ca