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Design and analysis report for the RL10-2B breadboard low thrust engineThe breadboard low thrust RL10-2B engine is described. A summary of the analysis and design effort to define the multimode thrust concept applicable to the requirements for the upper stage vehicles is provided. Baseline requirements were established for operation of the RL10-2B engine under the following conditions: (1) tank head idle at low propellant tank pressures without vehicle propellant conditioning or settling thrust; (2) pumped idle at a ten percent thrust level for low G deployment and/or vehicle tank pressurization; and (3) full thrust (15,000 lb.). Several variations of the engine configuration were investigated and results of the analyses are included.
Document ID
19850010710
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brown, J. R.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Foust, R. R.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Galler, D. E.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Kanic, P. G.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Kmiec, T. D.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Limerick, C. D.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Peckham, R. J.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Swartwout, T.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 5, 2013
Publication Date
December 12, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
FR-18046-3
NASA-CR-174857
NAS 1.26:174857
Accession Number
85N19020
Funding Number(s)
CONTRACT_GRANT: NAS3-24238
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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