NASA NTRS · 19900058640
Aeroassist Flight Experiment Reaction Control System preliminary design
Abstract
The 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.
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Langford, G. K., Price, D. E., Gallaher, M. W.. 1990-07-01. Aeroassist Flight Experiment Reaction Control System preliminary design. https://ntrs.nasa.gov/citations/19900058640
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