Approach to design is based upon use of residual atmosphere to achieve satellite orientation and to provide decelerating forces which effect re-entry and allow precise control of landing point; umbrella-like steel drag brake proposed by Avco-Everett Research Laboratory consists of ribs, covering material, actuating mechanism, and capsule; principle of operation and control system philosophy; terminal velocity; drag brake potential. (See also Astronautics v 4 n 7 July 1959 p 34-5, 90, 92, 95-6)
Drag brake for manned satellite recovery
Missiles Rockets
Missiles and Rockets ; 5 , n 26
1959
4 pages
Article (Journal)
English
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Drag brake for manned satellite recovery
Engineering Index Backfile | 1959
|NTIS | 1969
|Engineering Index Backfile | 1963
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