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COMBINED EFFECT OF CONTRACTION RATIO AND CHAMBER PRESSURE ON THE PERFORMANCE OF A GASEOUS-HYDROGEN-LIQUID-OXYGEN COMBUSTOR FOR A GIVEN PROPELLANT WEIGHT FLOW AND OXIDANT-FUEL RATIO

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BookPublisher: Nasa, Washington, D.C. 1961Description: 13.DDC classification: NASA | TN D-129

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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-129 (Browse shelf)	Not for loan		TR15637

Total holds: 0

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Previous	NASA TN D-1287 - EXPERIMENTAL INVESTIGATION OF WATER-ABSORBENT MATERIALS AS POSSIBLE HEAT SINKS FOR HYPERSONIC AND REENTRY VEHICLES	NASA TN D-1288 - ANALYTICAL INVESTIGATION OF PERFORMANCE OF TWO-STAGE TURBINE OVER A RANGE OF RATIOS OF SPECIFIC HEATS FROM 1.2 TO 1 AND 2/3	NASA TN D-1289 - ABSORPTION AND EMISSION CHARACTERISTICS OF DIFFUSE SPHERICAL ENCLOSURES	NASA TN D-129 COMBINED EFFECT OF CONTRACTION RATIO AND CHAMBER PRESSURE ON THE PERFORMANCE OF A GASEOUS-HYDROGEN-LIQUID-OXYGEN COMBUSTOR FOR A GIVEN PROPELLANT WEIGHT FLOW AND OXIDANT-FUEL RATIO	NASA TN D-1290 - ADDITION TO THE YALE TABLES FOR THE DEVELOPMENT OF THE DISTURBING FUNCTION	NASA TN D-1292 A PULSED FREQUENCY MODULATION DECOMMUTATOR	NASA TN D-1293 TELEMETERING INFRARED DATA FROM THE TIROS METEOROLOGICAL SATELLITES	Next

Bound With Nasa Tn D-121-128,130

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