NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Orbit Transfer Vehicle (OTV) engine, phase A study. Volume 1: Executive SummaryDesign and parametric data for the hydrogen oxygen engine used in the orbiter transfer vehicle are presented. The engine design is analyzed and minimum engine performance and man rating requirements are discussed. Candidate cycle performance, weight and tradeoff analysis, and cost estimates are reported.
Document ID
19790025064
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mellish, J. A. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 29, 1979
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-161297
REPT-32999-F-VOL-1
Report Number: NASA-CR-161297
Report Number: REPT-32999-F-VOL-1
Accession Number
79N33235
Funding Number(s)
CONTRACT_GRANT: NAS8-32999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available