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A PRELIMINARY STUDY OF THE USE OF FINITE-THRUST ENGINES FOR ABORT DURING LAUNCH OF SPACE VEHICLES

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BookPublisher: Nasa, Washington, D.C. 1961Description: 23.DDC classification: NASA | TN D-713

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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-713 (Browse shelf)	Not for loan		TR12614

Total holds: 0

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Previous	NASA TN D-7127 LOCAL HEAT-TRANSFER CHARACTERISTICS OF A ROW OF CIRCULAR AIR JETS IMPINGING ON A CONCAVE SEMICYLINDRICAL SURFACE.	NASA TN D-7128 EFFECTS OF A REDUCTION IN BLADE THICKNESS ON PERFORMANCE OF A SINGLE-STAGE 20.32-CENTIMETER MEAN-DIAMETER TURBINE.	NASA TN D-7129 FIRST-ORDER OPTICAL ANALYSIS OF A QUASI-MICROSCOPE FOR PLANETARY LANDERS.	NASA TN D-713 A PRELIMINARY STUDY OF THE USE OF FINITE-THRUST ENGINES FOR ABORT DURING LAUNCH OF SPACE VEHICLES	NASA TN D-7133 EVALUATION OF MAGNESIUM-LAUMINUM EUTECTIC TO IMPROVE COMBUSTION EFFICIENCY IN LOW BURNING-RATE PROPELLANTS.	NASA TN D-7134 ANALYSIS OF ELECTRICAL CONTACT OCCURRENCES BETWEEN ROLLING SURFACE WITH APPLICATION TO ELASTOHDRODNAMIC LUBRICATION.	NASA TN D-7135 COMPARISON OF COMBUSTION CHARACTERISTICS OF ASTM A-1,PROPANE.AND NATURAL-GAS FUELS IN AN ANNULAR TURBOJET COMBUSTOR.	Next

Bound With Nasa Tn D-701-12, 714-20

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