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Ignition of a hydrogen-oxygen rocket engine by addition of fluorine to the oxidant

By: R James Rollbuhler.

Contributor(s): David M Straight.

Material type: materialTypeLabel

materialTypeLabel

BookPublisher: DDC classification: NASA | TN D-1309 -

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-1309 - (Browse shelf)	Not for loan		TR9664

Total holds: 0

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Previous	NASA TN D-1304 - SECONDARY FLOW FIELDS EMBEDDED IN HYPERSONIC SHOCK LAYERS	NASA TN D-1305 - EMISSION SPECTRA FROM HIGH-PRESSURE HYDROGEN-OXYGEN COMBUSTION	NASA TN D-1308 - SURVEY OF ENERGY-ABSORPTION DEVICES FOR SOFT LANDING OF SPACE VEHICLES	NASA TN D-1309 - Ignition of a hydrogen-oxygen rocket engine by addition of fluorine to the oxidant	NASA TN D-1310 - OBSEVATION OF PROPERTIES OF SINTERED WROUGHT TUNGSTEN SHEET AT VERY HIGH TEMPERATURES	NASA TN D-1312 ANALYSIS OF MELTING BOUNDARY LAYERS ON DECELERATING BODIES.	NASA TN D-1313 EFFLUX OF THERMAL RADIATION FROM A CYLINDRICAL CAVITY IRRADIATED FROM AN EXTERNAL SOURCE	Next

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