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MODEL INVESTIGATION OF THE LANDING CHARACTERISTICS OF A REENTRY SPACECRAFT WITH A VERTICAL-CYLINDER AIR BAG FOR LOAD ALLEVIATION

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BookPublisher: Nasa,Washington, D.C. 1962Description: 38.DDC classification: NASA | TN D-1027

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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-1027 (Browse shelf)	Not for loan		TR10754

Total holds: 0

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Previous	NASA TN D-1024 MEASURED SURFACE DEFECTS ON TYPICAL TRANSONIC AIRPLANES AND ANALYSIS OF THEIR DRAG CONTRIBUTION	NASA TN D-1025 RECIEVING SYSTEM DESIGN FOR THE ARRAYING OF INDEPENDENTLY STEERABLE ANTENNAS FOR DEEP SPACE COMMUNICATION	NASA TN D-1026 WIND-TUNNE TEST OF A 1/20-SCALE AIRSHIP MODEL WITH STERN PROPELLERS	NASA TN D-1027 MODEL INVESTIGATION OF THE LANDING CHARACTERISTICS OF A REENTRY SPACECRAFT WITH A VERTICAL-CYLINDER AIR BAG FOR LOAD ALLEVIATION	NASA TN D-1028 CHARACTERISTIC OF THREE PRECISION CIRCUMLUNAR TRAJECTORIES FOR THE YEAR 1968	NASA TN D-1029 A STUDY OF THE OPTIMUM VELOCITY CHANGE TO INTERCEPT AND RENDEZVOUS	NASA TN D-1030 AN EXPERIMENTAL TECHNIQUE FOR THE INVESTIGATION OF TIPPOF FORCES ASSOCIATED WITH STAGE SAPARATION OF MULTISTAGE ROCKET VEHICLES	Next

Bound With Nasa Tn D-1021-1026 & 1028-1030

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