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STUDY OF THE USE OF TERMINAL CONTROL TECHNIQUES FOR GUIDENCE DURING DIRECT AND SKIP ENTRIES FOR A CAPSULE-TYPE VEHICLE AT PARABOLIC VELOCITY.

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BookPublisher: Nasa, Washington, D.C. 1964Description: 45.DDC classification: NASA | TN D-2055

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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-2055 (Browse shelf)	Not for loan		TR15579

Total holds: 0

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Previous	NASA TN D-2050 EFFECTS OF FLANK LOSSES IN THE THEORY OF SPACE-PROBE ENTRY UNDER CONDITIONS OF HIGH MASS LOSS.	NASA TN D-2052 THE DESIGN OF SAILPLANES FOR OPTIMUM THERMAL SOARING PERFORMANCE.	NASA TN D-2053 WIND-COMPENSATION METHOD AND RESULTS OF ITS APPLICATION TO FLIGHT TESTS OF TWELVE TRILBLAZER ROCKET VEHICLES.	NASA TN D-2055 STUDY OF THE USE OF TERMINAL CONTROL TECHNIQUES FOR GUIDENCE DURING DIRECT AND SKIP ENTRIES FOR A CAPSULE-TYPE VEHICLE AT PARABOLIC VELOCITY.	NASA TN D-2056 PHENOMENA OF PNEUMATIC TIRE HYDROPLANNING.	NASA TN D-2057 STATIC LONGITUDINAL CHRACTERISTICS OF THE PROJECT FIRE REENTRY STAGE AFTER REENTRY-PACKAGE SEPRATION AT MACH 28.3 IN HELIUM.	NASA TN D-2058 APPROXIMATE CALCULATION OF HYPERSONIC CONICAL FLOW PARAMETERS FOR AIR IN THERMODYNAMICS EQUILIBRIUM.	Next

Bound With Nasa Tn D-7051-7054,7056-7060.

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