Cooling of rocket thrust chambers with liquid oxygen
By: Elizabeth S. Armstrong and Julie A. Schlumberger ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.
Contributors: Schlumberger, Julie A.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 103146.
Publisher: NASA; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Rocket engines -- Thrust.; Combustion chambers.; Cooling.; Cracking (Fracturing); Engine coolants.; Fatigue (Materials); Liquid oxygen.; Liquid propellant rocket engines.; Oxygen-hydrocarbon rocket engines.; Rocket linings.; Thrust chambers.
Notes: Cover title.

Shipping list no.: 90-0893-M.

"AIAA-90-2120."

"E-5498"--P. 1.

Includes bibliographical references (p. 4).

Also available via Internet from the NASA Technical Report Server web site. Address as of 1/18/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900013289%5F1990013289.pdf; current access available via PURL.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

590-01-21.