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SEPS mission and system integration/interface requirements for the space transportation systemEarth escape mission requirements on Solar Electric Propulsion System (SEPS), and the interface definition and planned integration between SEPS, user spacecraft, and other elements of the STS. Emphasis is placed on the Comet rendezvous mission, scheduled to be the first SEPS user. Interactive SEPS interface characteristics with spacecraft and mission, as well as the multiple organizations and inter-related development schedules required to integrate the SEPS with spacecraft and STS, require early attention to definition of interfaces in order to assure a successful path to the first SEPS launch in July 1985
Document ID
19800032277
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cork, M. J. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Barnett, P. M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Shaffer, J., Jr. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Doran, B. J. (NASA Marshall Space Flight Center Systems Laboratory, Huntsville, Ala., United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1979
Subject Category
Astronautics (General)
Report/Patent Number
AAS PAPER 79-287
Meeting Information
Meeting: Annual Meeting
Location: Los Angeles, CA
Start Date: October 29, 1979
End Date: November 1, 1979
Sponsors: American Astronautical Society
Accession Number
80A16447
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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