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Large Diameter Shuttle Launched-AEM (LDSL-AEM) studyA technical description of a Large Diameter Shuttle Launched-AEM (LDSL-AEM), an AEM base module adapted to carry 5 ft diameter payloads in the shuttle with propulsion for carrying payloads to higher altitude orbits from a 150 NM shuttle orbit, is described. The AEM is designed for launch on the scout launch vehicle. Onboard equipment provides capability to despin, acquire the earth, and control the vehicle in an earth pointing mode using reaction wheels for torque with magnets for all attitude acquisition, wheel desaturation, and nutation damping. Earth sensors in the wheels provide pitch and roll attitude. This system provides autonomous control capability to 1 degree in pitch and roll and 2 degrees in yaw. The attitude can be determined to .5 degrees in pitch and roll and 2 degrees in yaw.
Document ID
19760023168
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
April 28, 1976
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-144797
D268-10656-1
Report Number: NASA-CR-144797
Report Number: D268-10656-1
Accession Number
76N30256
Funding Number(s)
CONTRACT_GRANT: NAS5-23537
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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