The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
By: Kenneth J. Kacynski and Joe D. Hoffman.
Contributors: Hoffman, Joe D., 1934-; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 106617.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Film cooling.; Flow distribution.; Heat transfer.; Hydrogen oxygen engines.; Nozzle flow.; Sweat cooling.; Thermal diffusion.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0807-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.