Physics
Scientific paper
Jan 1979
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979lock.reptv.....&link_type=abstract
Final Report Lockheed Missiles and Space Co., Sunnyvale, CA.
Physics
Electric Power Supplies, Mission Planning, Space Shuttle Payloads, Space Transportation, Systems Engineering, Attitude Control, Data Processing, Spaceborne Experiments, Spacelab Payloads, User Requirements
Scientific paper
The capability of the 25 kW power module to conduct representative missions which include Earth, solar, and stellar observation as well as zero-gravity experiments was assessed. Mission accommodations and related technical characteristics of the various operating modes are summarized. The minimum power module provides a substantial mission support on sortie flights. The addition of an attitude sensor is required for free-flying pointing missions.
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