DocumentCode
1175978
Title
Electroexplosive Devices in Aerospace Vehicle Systems
Author
Moses, Sidney A.
Author_Institution
Douglas Aircraft Company, Inc. Missile & Space Systems Division
Issue
4
fYear
1966
fDate
7/1/1966 12:00:00 AM
Firstpage
51
Lastpage
56
Abstract
Reasons for using electroexplosive devices in aerospace vehicles are given. A number of different electroexplosive devices are illustrated and their uses are described. The explosive materials used in these devices are discussed in two classes: propellants and high explosives. Methods for controlling deflagration or detonation to achieve desired effects are discussed. Construction of a typical electroexplosive cartridge is described, with special reference to the bridgewire-explosive system. A ??bridgewire equation?? is suggested for determining the functioning characteristics of the system. The method of determining the reliability of these ??one-shot?? items is compared to that used for devices which may be operated for a number of cycles. Safety of handling electroexplosive devices is discussed along with a few common-sense rules for accident prevention.
Keywords
Aerospace materials; Aircraft; Circuits; Electric shock; Electron tubes; Explosives; Missiles; Propellants; Pulse amplifiers; Vehicles;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1966.4501821
Filename
4501821
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