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Upper-stage space-shuttle propulsion by means of separate scramjet and rocket engines [NASA TN D-6762]

By: Francisus, Leo C.

Contributor(s): Allen, John L.

Material type: materialTypeLabel

materialTypeLabel

BookSeries: National Aeronautics and Space Administration [NASA]. Publisher: Washington, D.C. National Aeronautics and Space Administration [NASA] 1972Description: iv, 48p.Subject(s): Space-shuttle propulsionDDC classification: NASA | TN D-6762

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-6762 (Browse shelf)	Not for loan		TR015800

Total holds: 0

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Previous	NASA TN D-6750 DEVELOPMENT OF AN AIR FLOW THERMAL BALANCE CALORIMETER	NASA TN D-6760 Ring structure of a neutral gas cloud studied in a one-dimensional expansion into space [NASA TN D-6760]	NASA TN D-6760 Comparison of conventional and microasperity elastohydrodynamic lubrication of a ball spinning in nonconforming groove [NASA TN D-6761]	NASA TN D-6762 Upper-stage space-shuttle propulsion by means of separate scramjet and rocket engines [NASA TN D-6762]	NASA TN D-6763 Effect of casing boundary-layer removal on noise of a turbofan rotor [NASA TN D-6763]	NASA TN D-6764 Comparison of predicted and experimental heat-transfer and pressure-drop results for an air-cooled plug nozzle and supporting struts [TN D-6764]	NASA TN D-6765 Arched-outer-race ball-bearing analysis considering centrifugal forces [TN D-6765]	Next

Bound with NASA TN D-6760-6769

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