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Conceptual design of an orbital propellant transfer experiment. Volume 2: Study resultsThe OTV configurations, operations and requirements planned for the period from the 1980's to the 1990's were reviewed and a propellant transfer experiment was designed that would support the needs of these advanced OTV operational concepts. An overall integrated propellant management technology plan for all NASA centers was developed. The preliminary cost estimate (for planning purposes only) is $56.7 M, of which approximately $31.8 M is for shuttle user costs.
Document ID
19800022917
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Drake, G. L.
(General Dynamics/Convair San Diego, CA, United States)
Bassett, C. E.
(General Dynamics/Convair San Diego, CA, United States)
Merino, F.
(General Dynamics/Convair San Diego, CA, United States)
Siden, L. E.
(General Dynamics/Convair San Diego, CA, United States)
Bradley, R. E.
(General Dynamics/Convair San Diego, CA, United States)
Carr, E. J.
(General Dynamics/Convair San Diego, CA, United States)
Parker, R. E.
(General Dynamics/Convair San Diego, CA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1980
Subject Category
Astronautics (General)
Report/Patent Number
NASA-CR-165150
GDC-ASP-80-013-VOL-2
Report Number: NASA-CR-165150
Report Number: GDC-ASP-80-013-VOL-2
Accession Number
80N31423
Funding Number(s)
CONTRACT_GRANT: NAS3-21935
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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