Development and design of 2-ft diam cassegrain monopulse antenna assembly for Lunar Module Rendezvous Radar; radar will provide position and rate information on range and angles between Lunar Module and Command Service Module for navigation and guidance computations during lunar stay and ascent-rendezvous phases of Apollo Mission; controlling factors such as performance requirements, angular coverage, and envelope restrictions are discussed; principal design features are presented. (31001)
Tracking antenna for space rendezvous
ASME -- Aviation and Space -- Progress and Prospects
ASME -- Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Tracking
1968
6 pages
Conference paper
English
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