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EXPERIMENTAL EVALUATION OF SIX ABLATIVE-MATERIAL THRUST CHAMBERS AS COMPONENTS OF STORABLE-PROPELLANT ROCKET ENGINES

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BookPublisher: Nasa, Washington, D.C. 1967Description: 40.DDC classification: NASA | TN D-3945 -

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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-3945 - (Browse shelf)	Not for loan		TR9140

Total holds: 0

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Previous	NASA TN D-3942 - IMPROVING PERFORMANCE OF FACE CONTACT SEAL IN LIQUID SODIUM (400(DEGREE) TO 1000(DEGREE) F) BY INCORPORATION OF SPIRAL-GROOVE GEOMETRY	NASA TN D-3943 - ASSESSMENT OF CONVECTION, CONDUCTION, AND EVAPORATION IN NUCLEATE BOILING	NASA TN D-3944 - BRAZING TUNGSTEN FOR HIGH-TEMPERATURE NUCLEAR SERVICE IN HYDROGEN	NASA TN D-3945 - EXPERIMENTAL EVALUATION OF SIX ABLATIVE-MATERIAL THRUST CHAMBERS AS COMPONENTS OF STORABLE-PROPELLANT ROCKET ENGINES	NASA TN D-3947 - TIME-DEPENDENT STRUCTURE OF ONE-DIMENSIONAL MAGNETIC COMPRESSION WAVES IN COLLISIONLESS PLASMAS	NASA TN D-3948 - BEARING TORQUE AND FATIGUE LIFE STUDIES WITH SEVERAL LUBRICANTS FOR USE IN THE RANGE 500(DEGREE) TO (700) F	NASA TN D-3949 - HIGH-VOLTAGE CHARACTERISTICS OF A LARGE-GAP COAXIAL-CYLINDER ELECTRODE	Next

Bound With Nasa Tn D-3941-50

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