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STATIC STABILITY AND SEPRATION CHRACTERISTICS A TWO-STAGE ROCKET CONFIGURATION AT MACH NUMBERS FROM 1.57 TO 4.50.

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BookPublisher: Nasa, Washington, D.C. 1960Description: 35.DDC classification: NASA | TN D-188

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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-188 (Browse shelf)	Not for loan		TR15748

Total holds: 0

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Previous	NASA TN D-1877 - EXPERIMENTAL INVESTIGATION OF CHEMICAL REGENERATION OF SURFACES IN SIMULATED THERMIONIC DIODES	NASA TN D-1878 - EFFECT OF VARIABLE THERMAL PROPERTIES ON ONE-DIMENSIONAL HEAT TRANSFER IN RADIATING FINS	NASA TN D-1879 - THERMIONIC EMISSION FROM CESIUM-COATED ELECTROSTATIC ION-THRUSTER ELECTRODES	NASA TN D-188 STATIC STABILITY AND SEPRATION CHRACTERISTICS A TWO-STAGE ROCKET CONFIGURATION AT MACH NUMBERS FROM 1.57 TO 4.50.	NASA TN D-1880 - EFFECT OF TWO BRAZE COATINGS, PROCESSING VARIABLES, AND HEAT TREATMENTS ON 1200(DEGREE) F STRESS-RUPTURE STRENGTH OF L-605, A-286, AND INCONEL 700 SHEET	NASA TN D-189 STATIC-STABILITY MEASURENETS OF A STAND-ON TYPE HELICOPTER WITH RIGID BLADES, INCLUDING A COMPARISON WITH THEORY.	NASA TN D-190 EXPLORATORY INVESTIGATION OF SEVERAL COATED AND UNCOATED METAL, REFRACTORY, AND GRAPHICTE MODELS IN A 3,800 DEGREE F STAGNATION TEMPERATURE AIR JET.	Next

Bound With Nasa Tn D-181-187,189-190.

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