Technical paper presents derivation of approximate, closed-form equation for relationship between velocity of projectile and density of atmosphere. Results of calculations based on approximate equation agree well with results from numerical integrations of exact equations of motion. Comparisons of results presented in series of graphs.
Trajectory And Heating Of A Hypervelocity Projectile
NASA Tech Briefs ; 16 , 2
1992-02-01
Miscellaneous
No indication
English
Hypervelocity projectile technology (D2)
AIAA | 1992
|Hypervelocity Projectile Technology (D2)
AIAA | 1992
|The D2 hypervelocity projectile program
Tema Archive | 1995
|Initiation of Detonation by a Hypervelocity Projectile
AIAA | 1997
|Hypervelocity High Speed Projectile Imagery and Video
NTRS | 2009
|