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DESIGN AND PERFORMANCE OF A LIQUID-HYDROGEN, LIQUID-OXYGEN GAS GENERATOR FOR DRIVING A 1000-HORSEPOWER TURBINE.

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BookPublisher: Nasa, Washington, D.C. 1962Description: 28.DDC classification: NASA | TN D-1317

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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-1317 (Browse shelf)	Not for loan		TR10886

Total holds: 0

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Previous	NASA TN D-1313 EFFLUX OF THERMAL RADIATION FROM A CYLINDRICAL CAVITY IRRADIATED FROM AN EXTERNAL SOURCE	NASA TN D-1314 BOILING HEAT TRANSFER TO LIQUID HYDROGEN AND NITROGEN IN FORCED FLOW.	NASA TN D-1316 THREE-DIMENSIONAL TRAJECTORY ANALYSIS FOR ROUND-TRIP MISSION TO MARS	NASA TN D-1317 DESIGN AND PERFORMANCE OF A LIQUID-HYDROGEN, LIQUID-OXYGEN GAS GENERATOR FOR DRIVING A 1000-HORSEPOWER TURBINE.	NASA TN D-1318 PERFORMANCE OF SEVERAL CAST NICKLE-BASE ALLOYS AS TURBOJET-ENGINE BUCKET MATERIALS AT 1650 DEGREE F.	NASA TN D-1319 THREE-DIMENSIONAL TRAJECTORY ANALYSIS FOR ROUND-TRIP MISSION TO VENUS.	NASA TN D-1320 A CENTRAL FACILITY FOR RECORDING AND PROCESSING TRANSIENT-TYPE DATA .	Next

Bounds With Nasa Tn D-1311-16, 1318-1320 Lack No. 1315

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