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COLD PERFORMANCE EVALUATION OF A 4.59-INCH RADIAL-INFLOW TURBINE DESIGNED FOR A BRATON-CYCLE SPACE POWER SYSTEM

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BookPublisher: Nasa, Washington, D.C. 1966Description: 19.DDC classification: NASA | TN D-3260

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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-3260 (Browse shelf)	Not for loan		TR15522

Total holds: 0

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Previous	NASA TN D-3258 EXPERIMENTAL EVALUATION OF VARIOUS NONMETALLIC ABLATIVE MATERIALS AS NOZZLE SECTIONS OF HYDROGEN-OXYGEN ROCKET ENGINE	NASA TN D-3259 EVALUATION OF IMPREGNATED LUBRICANTS IN BALL-BEARING RETAINERS AT 10 TO THE POWER OF MINUS 6 TORR3	NASA TN D-326 LARGE-SCALE WIND-TUNNEL TESTS OF A WINGLESS VERTICAL TAKE-OFF AND LANDING AIRCRAFT- PRELIMINARY RESULTS.	NASA TN D-3260 COLD PERFORMANCE EVALUATION OF A 4.59-INCH RADIAL-INFLOW TURBINE DESIGNED FOR A BRATON-CYCLE SPACE POWER SYSTEM	NASA TN D-327 A TECHNIQUE FOR DETEMINING RELAXATION TIMES BY FREE- FLIGHT TESTS OF LOW- FINENESS- RATIO CONES; WITH EXPERIMENTAL RESULTS TEMERATURES UP TO 3440 DEGREE K	NASA TN D-3272 EXPERIMENTAL STUDY OF STAGNATION ENTHALPY IN THE LANGLEY HOTSHOT TUNNEL	NASA TN D-3273 AN ALGORITHM FOR SYNTHESIS OF SYNCHRONOUS SEQUENTIAL CIRCUITS	Next

Bound With Nasa Tn D-3251-59

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