DocumentCode
1502012
Title
System design
Author
Bowers, J. L.
Author_Institution
General Dynamics Corp, Convair-Astronautics, San Diego, Calif.
Volume
77
Issue
12
fYear
1958
Firstpage
1091
Lastpage
1092
Abstract
A GREAT DEAL OF ATTENTION is being paid to the celestial mechanics of space flight and the synthesis of systems to control space vehicles, satellites, and missiles. However, no less important is the problem of the practical design and construction of the vehicles and control hardware which will be required to realize our current potentialities in meeting the challenge of space travel. The scope of the discussion to follow will be restricted by omitting consideration of specific instruments, such as inertial components, platforms, etc., and concentrate on the over-all problem of electrical and mechanical design of parts, components, and systems. Consideration will be given to the physical design of control systems as well as power systems required to provide motivating energy. The attributes of reliability and accuracy will also be treated insofar as they affect the aforementioned topics.
Keywords
Aerospace electronics; Batteries; Control systems; Missiles; Power system reliability; Reliability; Space vehicles;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1958.6445498
Filename
6445498
Link To Document