High performance solid rocket motor (SRM) submerged nozzle-combustion cavity flowfield assessment
Subtitle: final report
By: prepared by J.A. Freeman ... [et al.]
Contributors: Freeman, Jon A; United States. National Aeronautics and Space Administration
Series: NASA contractor report -- NASA CR-179307
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1987
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Notes: Distributed to depository libraries in microfiche

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1988] 1 microfiche