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Liquid Rocket Propulsion Technology: An evaluation of NASA's programThe liquid rocket propulsion technology needs to support anticipated future space vehicles were examined including any special action needs to be taken to assure that an industrial base in substained. Propulsion system requirements of Earth-to-orbit vehicles, orbital transfer vehicles, and planetary missions were evaluated. Areas of the fundamental technology program undertaking these needs discussed include: pumps and pump drives; combustion heat transfer; nozzle aerodynamics; low gravity cryogenic fluid management; and component and system life reliability, and maintenance. The primary conclusion is that continued development of the shuttle main engine system to achieve design performance and life should be the highest priority in the rocket engine program.
Document ID
19810018653
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-164550
Accession Number
81N27191
Funding Number(s)
CONTRACT_GRANT: NASW-3455
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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