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CURVE FITS OF PREDICTED INVISCID STAGNATION-POINT RADIATIVE HEATING RATES, COOLING FACTORS, AND SHOCK STANDOFF DISTANCES FOR HYPERSONIC EARTH ENTRY

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BookPublisher: Nasa, Washington, D.C. 1974Description: 41.DDC classification: NASA | TN D-7622 -

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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-7622 - (Browse shelf)	Not for loan		TR7505

Total holds: 0

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Previous	NASA TN D-7618 - ADVERSE EFFECT OF FILM COOLING ON THE SUCTION SURFACE OF A TURBINE VANE	NASA TN D-7619 - EVALUATION OF TANTALUM-ALLOY-CLAD URANIUM MONONITRIDE FUEL SPECIMENS FROM 7500-HOUR, 1040[DEGREE] C PUMPED-LITHIUM-LOOP TEST	NASA TN D-762 INTERNAL-PERFORMANCE EVLUATION OF A TWO-POSITION DIVERGENT SHROUD EJECTOR	NASA TN D-7622 - CURVE FITS OF PREDICTED INVISCID STAGNATION-POINT RADIATIVE HEATING RATES, COOLING FACTORS, AND SHOCK STANDOFF DISTANCES FOR HYPERSONIC EARTH ENTRY	NASA TN D-7625 - TURBINE FOR A LOW-COST TURBOJET ENGINE	NASA TN D-7626 - TURBINE FOR ORDNANCE TURBOJET ENGINE	NASA TN D-7627 - SYSTEMATIC STUDY OF FOCAL RATIOS AND EFFECTS OF OPTICAL MISALIGNMENT FOR LST	Next

Bound With Nasa Tn D-7621-30

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