Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

An edition of Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber (1996)

Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber

By Mary F. Wadel

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Publish Date

1996

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: High aspect ratio, Rocket engines, Performance tests, Mass flow, Cooling, Thrust chambers, Combustion chambers, Liquid hydrogen