The science experiments for the Aeroassist Flight Experiment (AFE) will be greatly enhanced by taking measurements with no Reaction Control System (RCS) contamination just before perigee. Methods of modifying the AFE guidance to accomplish this are discussed. Several methods that could give up to 30 seconds of quiet time were investigated and the results of these guidance modifications shown. A 20 second quiet time is definitely possible and a 30 second quiet time may be possible if the guidance can be inactive past perigee. Some of the most significant being the criterion for determining if the mission is threatened. A limited follow-on test program is outlined.
Aeroassist Flight Experiment Guidance Quiet Time
1988
78 pages
Report
Keine Angabe
Englisch
Aeroassist flight experiment guidance Quiet Time
NTRS | 1988
|The Aeroassist Flight Experiment
NTRS | 1987
|Aeroassist Flight Experiment (AFE)
NTRS | 1988
|Aeroassist Flight Experiment (AFE)
NTIS | 1988
|