Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-179595.
Publisher: Pratt and Whitney Aircraft; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1989
Place of publication: [West Palm Beach, Fla; Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: 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.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 2 microfiches.