Solid explosive detonation in direct contact with a metal body is examined to determine the energy transfer from latent chemical energy of an explosive into kinetic energy of the neighboring body structural members and spacecraft. Much of this is of an empirical nature since the time-dependent, three-dimensional problem involves extremely difficult analysis. Acoustic experiments were performed on a partially constructed spacecraft. A complete set of sound intensity maps was obtained.
Apollo Launch Escape Tower Electroexplosive Bolts
IEEE Transactions on Aerospace and Electronic Systems ; AES-2 , 5 ; 511-525
1966-09-01
3201597 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Development of the Apollo launch escape system.
NTRS | 1968
|Development of the Apollo launch escape system.
AIAA | 1968
|Development of the Apollo launch escape system
AIAA | 1967
|