Phase measurement/display subsystem for the Apollo re-entry tracking system
Abstract
A combined system consisting of an Interferometer and a Range System has been proposed (Reference #1) for tracking the Apollo spacecraft during the re-entry phase. The system herein discussed processes the output of the above system and performs the following functions.
Description
"X-531-63-251, NASA,Goddard Space Flight Center, Maryland, December 13, 1963"
Date
1963-12-13
Keywords
Interferometry , Tracking Control Systems , Apollo 1
Citation
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Publisher
NASA