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INFLUENCE OF HIGH-TURBINE-INLET-TEMPERATURE ENGINES IN A METHANE-FUELED SST WHEN TAKEOFF JET NOISE LIMITS ARE CONSIDERED

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BookPublisher: Nasa, Washington, D.C. 1968Description: 56.DDC classification: NASA | TN D-4965

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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-4965 (Browse shelf)	Not for loan		TR15830

Total holds: 0

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Previous	NASA TN D-4962 EXAMPLES OF CODING SCHEMES BASED ON STRATEGIC VALUE	NASA TN D-4963 THE INFLUENTIAL ASPECTS OF ATMOSPHERIC DISTURBANCES ON SPACE VEHICLES DESIGN USING STATISTICAL APPROACHES FOR ANALYSIS	NASA TN D-4964 DEVELOPMENT OF IMPROVED THROAT INSERTS FOR ABLATIVE ROCKET ENGINES	NASA TN D-4965 INFLUENCE OF HIGH-TURBINE-INLET-TEMPERATURE ENGINES IN A METHANE-FUELED SST WHEN TAKEOFF JET NOISE LIMITS ARE CONSIDERED	NASA TN D-4967 AN ANALYTICAL METHOD FOR PREDICTING THE PERFORMANCE OF CENTRIFUGAL PUMPS DURING PRESSURIZED STARTUP	NASA TN D-4968 INTERIM SUMMARY OF LIQUID ROCKET ACOUSTIC-MODE-INSTABILITY STUDIES AT A NOMINAL THRUST OF 20 000 POUNDS	NASA TN D-4969 A MATHEMATICAL ANALYSIS OF SUPERSONIC INLET DYNAMICS	Next

Bound With Nasa Tn D-4961-4964,4966-4970

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