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DESIGN AND EVALUATION OF AN OXIDANT-FUEL-RATIO-ZONED ROCKET INJECTOR FOR HIGH PERFORMANCE AND ABLATIVE ENGINE COMPATIBILITY

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BookPublisher: Nasa, Washington, D.C. 1972Description: 57.DDC classification: NASA | TN D-6918

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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-6918 (Browse shelf)	Not for loan		TR15250

Total holds: 0

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Previous	NASA TN D-6915 BOUNDARY LUBRICATION OF FORMULATED C-ETHERS IN AIR TO 300 DEGREE CENTIGRATE	NASA TN D-6916 COOLANT PRESSURE AND AIRFLOW DISTRIBUTION IN A STRUT-SUPPORTED TRANSPIRATION-COOLED VANE FOR A GAS TURBINE ENGINE	NASA TN D-6917 ANALYTICAL STUDY OF EFFECT OF CASING TREATMENT ON PERFORMANCE OF A MULTISTAGE COMPRESSOR	NASA TN D-6918 DESIGN AND EVALUATION OF AN OXIDANT-FUEL-RATIO-ZONED ROCKET INJECTOR FOR HIGH PERFORMANCE AND ABLATIVE ENGINE COMPATIBILITY	NASA TN D-6919 LOW SPEED AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE MODEL WITH A THIN, HIGHLY SWEPT, 2.67 ASPECT RATIO WING HAVING A CRANKED LEADING EDGE	NASA TN D-6931 - EFFECTS OF EXPERIMENTALLY MEASURED PRESSURE OSCILLATIONS ON THE VIBRATION OF A SOLID ROCKET MOTOR	NASA TN D-6932 - THREE-TRACK RUNWAY AND TAXIWAY PROFILES MEASURED AT INTERNATIONAL AIRPORTS I AND J	Next

Bound With Nasa Tn D-6910-6917,6919

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