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PERFORMANCE OF A SHORT MODULAR TURBOJET COMBUSTOR SEGMENT USING ASTM-A1 FUEL

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BookPublisher: Nasa, Washington, D.C. 1971Description: 32.DDC classification: NASA | TN D-6167

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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-6167 (Browse shelf)	Not for loan		TR13034

Total holds: 0

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Previous	NASA TN D-6164 DESIGN STUDY OF SHAFT FACE SEAL WITH SELF-ACTING LIFT AUGMENTATION	NASA TN D-6165 PRELIMINARY FRICTION AND WEAR STUDIES OF COBALT-RHENIUM SOLID SOLUTION ALLOY IN AIR AND IN VACUUM	NASA TN D-6166 FREQUENCY RESPONSE OF TWO TYPES OF LIQUID-METAL PRESSURE TRANSDUCERS WITH STANDOFF TUBES	NASA TN D-6167 PERFORMANCE OF A SHORT MODULAR TURBOJET COMBUSTOR SEGMENT USING ASTM-A1 FUEL	NASA TN D-6168 THE GAS PHASE IN POROUS FUEL-CELL ELECTRODES	NASA TN D-6169 NEUTRONIC DESIGN FOR A LITHIUM-COOLED REACTOR FOR SPACE APPLICATIONS	NASA TN D-618 - EXTENSION OF BOUNDARY-LAYER-SEPARATION CRITERIA TO A MACH NUMBER OF 6.5 BY UTILIZING FLAT PLATES WITH FORWARD-FACING STEPS	Next

Bound With Nasa Tn D-6160-6166,6168-6169

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