Research Catalog

Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle

Title
Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle [microform].
Author
Marable, R. W.
Publication
[West Palm Beach, Fla. : Pratt and Whitney Aircraft ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]

Details

Additional Authors
United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA contractor report ; NASA CR-179595
Subject
  • Combustion chambers
  • Engine tests
  • Fabrication
  • Hydrogen oxygen engines
  • Nozzle design
  • Performance tests
  • Propulsion system performance
  • Reusable rocket engines
  • RL-10 engines
  • Rocket engine design
  • Rocket nozzles
  • Specific impulse
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:179595
OCLC
marcive32623520
Author
Marable, R. W.
Title
Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle [microform].
Imprint
[West Palm Beach, Fla. : Pratt and Whitney Aircraft ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
Series
NASA contractor report ; NASA CR-179595
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 2 microfiches.
Added Author
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:179595
Research Call Number
READEX Microfiche NAS 1.26:179595
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