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PERFORMANCE ESTIMATES FOR SPACE SHUTTLE VEHICLES USING A HYDROGEN OR A METHANE-FUELED TURBORAMJET-POWERED FIRST STAGE

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BookPublisher: Nasa, Washington, D.C. 1972Description: 31.DDC classification: NASA | TN D-6634 -

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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-6634 - (Browse shelf)	Not for loan		TR8915

Total holds: 0

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Previous	NASA TN D-6631 - EFFECTS OF 22-MEV PROTONS ON SINGLE JUNCTION AND SILICON CONTROLLED RECTIFIERS	NASA TN D-6632 - SHORT-TERM HOT HARDNESS CHARACTERISTICS OF ROLLING-ELEMENT STEELS	NASA TN D-6633 - ANALYSIS AND COMPARISON OF WALL COOLING SCHEMES FOR ADVANCED GAS TURBINE APPLICATIONS	NASA TN D-6634 - PERFORMANCE ESTIMATES FOR SPACE SHUTTLE VEHICLES USING A HYDROGEN OR A METHANE-FUELED TURBORAMJET-POWERED FIRST STAGE	NASA TN D-6635 - REFRACTIVE INDEX AND BIREFRINGENCE OF 2H SILICON CARBIDE	NASA TN D-6636 - NOISE PRODUCED BY A SMALL-SCALE, EXTERNALLY BLOWN FLAP	NASA TN D-6637 - EFFECTS OF TRAILING-EDGE GEOMETRY AND THICKNESS ON THE PERFORMANCE OF CERTAIN TURBINE STATOR BLADING	Next

Bound With Nasa Tn D-6630-39

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