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.
Aeroassist Flight Experiment Reaction Control System preliminary design
01.07.1990
Aufsatz (Konferenz)
Keine Angabe
Englisch
The Aeroassist Flight Experiment
NTRS | 1987
|Aeroassist Flight Experiment (AFE)
NTRS | 1988
|Aeroassist Flight Experiment (AFE)
NTIS | 1988
|