Combustion of solid fuel slabs with gaseous oxygen in a hybrid motor analog
By: Martin J. Chiaverini ... [et al.].
Contributors: Chiaverini, Martin J.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA-CR-201116.; NASA contractor report -- NASA CR-201116.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Hybrid propellant rocket engines.; Laminar boundary layer.; Polybutadiene.; HTPB propellants.; Surface temperature.; Oxygen.; Pressure oscillations.; Combustion physics.; Turbulent combustion.; Propulsion system performance.
Notes: Shipping list no.: 98-0846-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.