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Aeroassist Flight Experiment Reaction Control System preliminary designThe Aeroassist Flight Experiment (AFE) has several different flight modes associated with its mission. The effect the spacecraft attitude control system (ACS) has on the Reaction Control System (RCS) requirements for all the flight modes is discussed. The ACS requirements and their consequences on the design of the RCS is then discussed in detail. Special problems in the RCS design unique to the AFE mission and the design solutions to these problems are presented.
Document ID
19900058640
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Langford, G. K. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Price, D. E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Gallaher, M. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 90-2763
Accession Number
90A45695
Distribution Limits
Public
Copyright
Other

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