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Solar Concentrator Conceptual Design for the /SUS Advanced Technology DemonstrationAn Integrated Solar Upper stage would permit such realignment to smaller vehicles but would also change the current expendable stage paradigm to a reusable one. ISUS would remain with the satellite following orbit insertion and function as its electrical power and propulsion subsystems. Since a satellite's power subsystem represents as much as 30% of its total mass, using the upper stage to replace an onboard photovoltaic/battery system will purchase additional mass for sensors and communication packages. The timely demonstration of an ISUS system, before the turn of the century, will permit such devices to be fielded in the early 2000's and in time to fly aboard major satellite block changes.
Document ID
20240006834
Acquisition Source
Glenn Research Center
Document Type
Contractor or Grantee Report
Authors
Charles H. Castle
(ANALEX Corporation)
Date Acquired
May 28, 2024
Publication Date
July 25, 1995
Subject Category
Spacecraft Propulsion and Power
Report/Patent Number
ER 1012
Funding Number(s)
CONTRACT_GRANT: NAS3-25776
CONTRACT_GRANT: Subcontract AC-95-3
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
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