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SERT D spacecraft studyThe SERT D (Space Electric Rocket Test - D) study defines a possible spacecraft project that would demonstrate the use of electric ion thrusters for long-term (5 yr) station keeping and attitude control of a synchronous orbit satellite. Other mission objectives included in the study were: station walking to satellite rendezvous and inspection, use of low cost attitude sensing system, use of an advanced solar array orientation and slip ring system, and an ion thruster integrated directly with a solar array power source. The SERT D spacecraft, if launched, will become SERT 3 the third space electric thruster test.
Document ID
19740007433
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-71494
Report Number: NASA-TM-X-71494
Accession Number
74N15546
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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