A comparison of analytical results for 20 K LOX/hydrogen instabilities
By: Mark D. Klem and Kevin J. Breisacher ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.
Contributors: Breisacher, Kevin J.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 103166.
Publisher: NASA; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 15
Subjects: Liquid propellants -- Combustion -- Computer simulation.; Liquid propellant rockets -- Computer simulation.; Combustion stability.; Computer programs.; Fuel injection.; Hydrogen oxygen engines.; Rocket engines.
Notes: Cover title.

Shipping list no.: 90-1086-M.

"AIAA-90-2241."

"E-5538"--P. 1.

Includes bibliographical references (p. 7).

Also available via Internet from the NASA Technical Report Server web site. Address as of 4/14/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900015870%5F1990015870.pdf; current access available via PURL.

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

582-01-21.