DocumentCode :
1176956
Title :
Apollo Launch Escape Tower Electroexplosive Bolts
Author :
Coffman, Samuel W. ; Nussberger, Arthur A.
Author_Institution :
Space and Information Systems Div. North American Aviation Inc. Downey, Calif.
Issue :
5
fYear :
1966
Firstpage :
511
Lastpage :
525
Abstract :
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.
Keywords :
Aerodynamics; Chemicals; Electric shock; Explosives; Fasteners; Kinetic energy; Poles and towers; Solids; Space vehicles; Temperature; Acoustic; Apollo; bolts; electroexplosive; explosive; launch; launch tower; spacecraft;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1966.4501927
Filename :
4501927
Link To Document :
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