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STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL CONFIGURATIONS USED IN THE DEVELOPMENT OF THE LITTLE JOE II-APOLLO TEST VEHICLE AT MACH NUMBERS FROM 0.056 TO 4.65

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BookPublisher: Nasa, Washington, D.C. Description: 213.DDC classification: NASA | TN D-4439

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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-4439 (Browse shelf)	Not for loan		TR15259

Total holds: 0

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Previous	NASA TN D-4435 DETERMINATION OF INTERSECTION OF PARTICLE FLIGHT PATH WITH SURFACE OF HELICAL TUBULAR VOID REGION	NASA TN D-4437 EFFECT OF TWO-DIMENSIONAL MULTIPLE SINE-WAVE PROTRUSIONS ON THE PRESSURE AND HEAT-TRANSFER DISTRIBUTIONS FOR A FLATE PLATE AT MACH 6	NASA TN D-4438 PROPOSED ANALYTICAL MODEL FOR THE FINAL STAGES OF LANDING A TRANSPORT AIRPLANE	NASA TN D-4439 STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL CONFIGURATIONS USED IN THE DEVELOPMENT OF THE LITTLE JOE II-APOLLO TEST VEHICLE AT MACH NUMBERS FROM 0.056 TO 4.65	NASA TN D-4440 EXPERIMENTS ON STABILITY OF HERRINGBONR-GROOVED GAS-LUBRICATED JOURNAL BEARINGS TO HIGH COMPRESSIBILITY NUMBERS	NASA TN D-4482 EXTERNAL AERODYNAMICS OF THE MAGNETOSPHERE	NASA TN D-4483 DETERMINING THE SPIN AXIS OF A SPINNING SATELLITE	Next

Bound With Nasa Tn D-4431-38,4440

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