Analysis of a rocket based combined cycle engine during rocket only operation
By: T.D. Smith ... [et al.].
Contributors: Smith, T. D.; Lewis Research Center.
Series: NASA/TM -- 1998-206639/REV1.; NASA technical memorandum -- 206639.
Publisher: National Aeronautics and Space Administration, Lewis Research Center; National Technical Information Service, distributor
Published: 1998
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Thrust chambers.; Thermodynamic cycles.; Specific impulse.; Rocket engines.; Pressure ratio.; Gas generators.; Ejectors.
Notes: Shipping list no.: 99-0559-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.