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1. FLIGHT TEST OF A 15-FOOT-DIAMETER (4.6-METER) 120[DEGREE] CONICAL SPACECRAFT SIMULATING PARACHUTE DEPLOYMENT IN A MARS ATMOSPHERE

by Darnell,Wayne L, Henning,Allen B | Lundstrom,Reginald R.

Material type: book Book Description: 74.Publisher: Nasa, Washington, D.C. 1967Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4266 -] (1).

2. ANALYTICAL INVESTIGATION OF A FLIKER-TYPE ROLL CONTROL FOR A MACH NUMBER 6 MISSILE WITH AERODYNAMIC CONTROLS OVER AN ALTITUDE RANGE OF 82,000 TO 282,000 FEET

by Lundstrom,Reginald R | Whitman,Ruth I.

Material type: book Book Description: 50.Publisher: Nasa, Washington, D.C. 1959Availability: No items available Damaged (1).

3. WIND-COMPENSATION METHOD AND RESULTS OF ITS APPLICATION TO FLIGHT TESTS OF TWELVE TRILBLAZER ROCKET VEHICLES.

by Henning,Allen B,Lundstrom,Reginald R | Keating,Jean C.

Material type: book Book Description: 81.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2053] (1).

4. FLIGHT TEST OF AN ERECTABLE SPACECRAFT USED FOR DECELERATOR TESTING AT SIMULATED MARS ENTRY CONDITIONS

by HENNING,ALLEN B | LUNDSTROM,REGINALD R.

Material type: book Book Description: ,57.Publisher: NASA, WASHINGTON, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6910] (1).

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