Atmosphere entries with spacecraft lift-drag ratios modulated to limit decelerations / Lionel L. Levy Jr.

Survey of energy-absorption devices for soft landing of space vehicles /

Esgar, Jack B.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Materials, eng...

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

Charczenko, Nickolai.
McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 /

Peterson, Victor L.
McKenzie, Robert L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Atmosphere entries with vehicle lift-drag ration modulated to limit deceleration and rate of deceleration: vehicles with maximum lift-drag ration of 0.5 /

Katzen, Elliott D.
Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bi...

The use of drag modulation to limit the rate at which deceleration increases during nonlifting entry /

Levy, Lional L.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry; Space mec...

An approximate analytical method for studying atmosphere entry of vehicles with modulated aerodynamic forces /

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Comparison of two maneuvers for longitudinal range control during atmospheric entry /

Levy, Lionel L.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."Januery 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond.

Spencer, Bernard.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Satellite...

Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Free-flight of fifth-stage entry vehicle at mach numbers of 5 and 17 /

Kirk, Donn B.
Miller, Robert J.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Stability a...

Analysis of melting boundary layers on decelerating bodies /

Ostrach, Simon.
Hamman, Jesse.
Goldstein, Arthur W.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Preliminary studies of manned satellites wingless configuration : nonlifting /

Faget, Maxime A. (Maxime Allan), 1921-2004.
Buglia, James J.
Garland, Benjamine J.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibli...

One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle /

Wells, William R.
McLellan, Charles H.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

Ware, George M.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Numerical analysis of the transient responce of advanced thermal protection systems for atmosphereic entry / Robert T. Swann and Claud M. Pittman.

Swann, Robert T.
Pittman, C. M. (Claud M.)
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Survey of energy-absorption devices for soft landing of space vehicles /

Esgar, Jack B.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Materials, eng...

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

Charczenko, Nickolai.
McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 /

Peterson, Victor L.
McKenzie, Robert L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Atmosphere entries with vehicle lift-drag ration modulated to limit deceleration and rate of deceleration: vehicles with maximum lift-drag ration of 0.5 /

Katzen, Elliott D.
Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bi...

The use of drag modulation to limit the rate at which deceleration increases during nonlifting entry /

Levy, Lional L.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Atmospheric entry; Space mec...

An approximate analytical method for studying atmosphere entry of vehicles with modulated aerodynamic forces /

Levy, Lionel L.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Comparison of two maneuvers for longitudinal range control during atmospheric entry /

Levy, Lionel L.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."Januery 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bib...

Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond.

Spencer, Bernard.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Satellite...

Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Free-flight of fifth-stage entry vehicle at mach numbers of 5 and 17 /

Kirk, Donn B.
Miller, Robert J.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Stability a...

Analysis of melting boundary layers on decelerating bodies /

Ostrach, Simon.
Hamman, Jesse.
Goldstein, Arthur W.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Preliminary studies of manned satellites wingless configuration : nonlifting /

Faget, Maxime A. (Maxime Allan), 1921-2004.
Buglia, James J.
Garland, Benjamine J.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibli...

One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle /

Wells, William R.
McLellan, Charles H.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mecha...

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

Ware, George M.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Numerical analysis of the transient responce of advanced thermal protection systems for atmosphereic entry / Robert T. Swann and Claud M. Pittman.

Swann, Robert T.
Pittman, C. M. (Claud M.)
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanic...

Survey of energy-absorption devices for soft landing of space vehicles /

Esgar, Jack B.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Materials, eng...

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

Charczenko, Nickolai.
McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 /

Peterson, Victor L.
McKenzie, Robert L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Atmosphere entries with spacecraft lift-drag ratios modulated to limit decelerations / Lionel L. Levy Jr.

Abstract

Extracted data

Atmosphere entries with spacecraft lift-drag ratios modulated to limit decelerations / Lionel L. Levy Jr.

Abstract

Extracted data

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