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Solar electric propulsion - A versatile stage for earth orbiting missionsThe paper examines recent developments in solar array and ion propulsion systems which make possible the utilization of readily available solar energy for spacecraft propulsion and operation. The Solar Electric Propulsion System (SEPS) stage represents a substantial increase in capability to perform interplanetary and earth orbiting missions due to the combination of high performance and low thrust. SEPS is an important augmentation to the Space Transportation System (STS) for numerous earth orbit missions because it can deliver a greatly increased total satellite mass to a geosynchronous orbit or greatly increase the on-orbit delta V capability.
Document ID
19800057597
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, D. D.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Webb, E. D.
(Lockheed Missiles and Space Co., Inc. Sunnyvale, Calif., United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1980
Subject Category
Astronautics (General)
Report/Patent Number
DGLR PAPER 80-095
LMSC-D758135
Report Number: DGLR PAPER 80-095
Report Number: LMSC-D758135
Meeting Information
Meeting: Symposium on Shuttle/Spacelab - The New Transportation System and its Utilization
Location: Hanover
Start Date: April 28, 1980
End Date: April 30, 1980
Sponsors: Deutsche Gesellschaft fuer Luft- und Raumfahrt and American Astronautical Society
Accession Number
80A41767
Funding Number(s)
CONTRACT_GRANT: NAS8-33754
Distribution Limits
Public
Copyright
Other

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