Design problems of very light radar equipment that will help guide 2-man spacecraft into rendezvous with orbiting target satellite are discussed; target enhancement; system accuracy; system characteristics; angle measurements; astronaut display.
Gemini rendezvous radar
Westinghouse Engr
Westinghouse Engineer ; 24 , n 1
1964
5 pages
Article (Journal)
English
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Engineering Index Backfile | 1965
|AIAA | 1963
|Engineering Index Backfile | 1964
|Gemini rendezvous radar system design
Engineering Index Backfile | 1966
|AIAA | 1966
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