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