High-temperature, oxidation-rersistant thruster research
By: prepared by J.R. Wooten, P.T. Lansaw.
Contributors: Lansaw, P. T.; Aerojet TechSystems Company (U.S.); Lewis Research Center.
Series: NASA CR -- 185233.; NASA contractor report -- NASA CR-185233.
Publisher: Aerojet Propulsion Division, Research & Technology; National Aeronautics & Space Administration, Lewis Research Center
Published: 1990
Place of publication: Sacramento, Calif; Cleveland, Ohio
Language: eng
Format: Microform
Subjects: Engine tests.; High temperature research.; Iridium.; Liquid propellant rocket engines.; Liquid rocket propellants.; Oxidation resistance.; Propulsion.; Protective coatings.; Temperature control.; Thrust chambers.; Vapor deposition.
Other titles: High temperature, oxidation resistant thruster research.
Notes: Also available via Internet from the NASA Technical Report Server web site. Address as of 5/9/06: http://ntrs.nasa.gov/archive/nasa/casi/ntrs.nasa.gov/19910006750%5F1991006750.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991]. 3 microfiches.