Principles employed in development of aerospace ground checkout and launch control equipment for use on Apollo and Gemini programs; PACE-S/C system is composed of PCM ground station subsystem, computing subsystem, display and control subsystem, data transmission subsystem, and spacecraft associated subsystem; details of each system and 3 modes of operation; primary method of real-time data display utilized is crt system which displays engineering data from computing complex in alphanumeric form.
PACE -- Preflight acceptance checkout equipment
Astronautics Aerospace Eng
Astronautics and Aerospace Engineering ; 1 , n 6
1963
3 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
PACE- PREFLIGHT ACCEPTANCE CHECKOUT EQUIPMENT
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