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Launch vehicle integration requirements for SP-100SP-100 is the designation for a nuclear reactor-based power plant being developed for both civil and military missions beginning in the 1990s for such potential space applications as communication satellites, space radar, electric propulsion and space stations. Typically, a system using the SP-100 along with a selected upper stage system would be launched by the National Space Transportation System (NSTS) Space Shuttle System into a near-earth orbit, deployed, and through upper stage propulsion burn(s) be inserted/transferred to its mission orbit. The nature of the advanced design SP-100 gives rise to a set of issues that require special attention to assure that payloads using this power plant are physically and functionally compatible with the NSTS and meet the safety requirements thereof. The purpose of this document is to define and present the requirements and interface provisions that, when satisfied, will ensure technical compatibility between SP-100 systems and the NSTS.
Document ID
19950002393
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shaw, L. T., Jr.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Womack, J. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 31, 1984
Subject Category
Nuclear And High-Energy Physics
Report/Patent Number
NASA-CR-196470
DE94-051276
JPL/D-1069
NAS 1.26:196470
Report Number: NASA-CR-196470
Report Number: DE94-051276
Report Number: JPL/D-1069
Report Number: NAS 1.26:196470
Accession Number
95N70513
Funding Number(s)
CONTRACT_GRANT: DE-AI03-86SF-16013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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