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COLD-AIR PERFORMANCE EVALUATION OF SCALE MODEL OXIDIZER PUMP-DRIVE TURBINE FOR THE M-1 HYDROGEN-OXYGEN ROCKET ENGINE : IV - PERFORMANCE OF FIRST STAGE WITH MODIFIED INLET FEEDPIPE-MANIFOLD ASSEMBLY

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BookPublisher: Nasa, Washington, D.C. 1968Description: 22.DDC classification: NASA | TN D-4393 -

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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-4393 - (Browse shelf)	Not for loan		TR10262

Total holds: 0

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Previous	NASA TN D-439 AXIAL-LOAD FATIGUE TESTS ON 17-7 PH STAINLESS STEEL UNDER CONSTANT-AMPLITUDE LOADING.	NASA TN D-4390 APPLICATION OF DIRECTIONAL SOLIDIFICATION TO A NASA NICKEL-BASE ALLOY (TAZ-8B)	NASA TN D-4392 - COLD-AIR PERFORMANCE EVALUATION OF SCALE MODEL OXIDIZER PUMP-DRIVE TURBINE FOR THE M-1 HYDROGEN-OXYGEN ROCKET ENGINE	NASA TN D-4393 - COLD-AIR PERFORMANCE EVALUATION OF SCALE MODEL OXIDIZER PUMP-DRIVE TURBINE FOR THE M-1 HYDROGEN-OXYGEN ROCKET ENGINE	NASA TN D-4394 - INVESTIGATION OF LEAKAGE OF LARGE-DIAMETER O-RING SEALS ON SPACECRAFT AIR-LOCK HATCHES	NASA TN D-4395 - WIND DATA FROM THE 250-FOOT (76.2-METER) TOWER AT WALLOPS ISLAND, VIRGINIA	NASA TN D-4396 - PILOTED SIMULATOR STUDY OF TAKEOFF PERFORMANCE AND HANDLING QUALITIES OF A DOUBLE-DELTA SUPERSONIC TRANSPORT	Next

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