Water landing impact accelerations for three models of reentry capsules /

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Experimental investigation of water-absorbent materials as possible heat sinks for hypersonic and reentry vehicles Robert P. Dengler and Reeves P. Cochran.

Dengler, Robert P.
Cochran, Reeves P.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aircraft; Atmospheric entry; Fluid mechanics; Materials, other; Structures.I...

Landing-impact characteristics of load-alleviating struts on a model of a winged space vehicle /

Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Space vehicles; Stresses and loads.Includes bibliographical references.Mo...

Investigation of the landing characteristics of a reentry vehicle having a canted multiple-air-bag load-alleviation system /

Stubbs, Sandy M.
McGehee, John R.
United States. National Aeronautics and Space Administration.

Cover title."August 1963."Includes bibliographical references.Mode of access: Internet

Water-landing characteristics of a 1/10-scale model of a winged missile /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Landing energy dissipation for manned reentry vehicles /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Includes bibliographical references.Mode of access: Internet

Effect of a load-alleviating structure on the landing behavior of a reentry-capsule model /

Hoffman, Edward L.
McGehee, John R.
Stubbs, Sandy M.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

Model investigation of the landing characteristics of a reentry spacecraft with a vertical-cylinder air bag for load alleviation /

McGehee, John R.
Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Space vehicles.Includes bibliogr...

Landing characteristics of a lentiucular-shaped reentry vehicle /

Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Major NASA subject terms:Space vehicles; Stresses and loads.Includes bi...

Water landing characteristics of a model of a winged reentry vehicle /

Stubbs, Sandy M.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 10.Mode of access: Internet

A concept of a manned satellite reentry which is completed with a glide landing /

Cheatham, Donald C.
United States. National Aeronautics and Space Administration.
Langley Research Center. Flight Research Division.

December 1959."Cover title.Includes bibliographical references (p. 25).Mode of access: Internet

Analytical investigation of the dynamic behavior of a nonlifting manned reentry vehicle. /

Lichtenstein, Jacob H.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Includes bibliographical references.Mode of access: Internet

Limited investigation of crushable structures for acceleration protection of occupants of vehicles at low impact speeds /

O'Bryan, Thomas C.
Hatch, Howard G.
United States. National Aeronautics and Space Administration.

Cover title."October 1959."Loads, landing, impact; Loads, landing, impact, land; Safety;Operating pr...

Hydrodynamic and aerodynamic characteristics of a model of a supersonic multijet water-based aircraft equipped with supercavitating hydrofoils /

McKann, Robert E.
Pearson, Albin O.
Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

A brief investigation of the effect of waves on the take-off resistance of a seaplane /

Mottard, Elmo J.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Hydrodynamic configurations, general; Hulls, seaplane, length-beam ratio...

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Experimental investigation of water-absorbent materials as possible heat sinks for hypersonic and reentry vehicles Robert P. Dengler and Reeves P. Cochran.

Dengler, Robert P.
Cochran, Reeves P.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aircraft; Atmospheric entry; Fluid mechanics; Materials, other; Structures.I...

Landing-impact characteristics of load-alleviating struts on a model of a winged space vehicle /

Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Space vehicles; Stresses and loads.Includes bibliographical references.Mo...

Investigation of the landing characteristics of a reentry vehicle having a canted multiple-air-bag load-alleviation system /

Stubbs, Sandy M.
McGehee, John R.
United States. National Aeronautics and Space Administration.

Cover title."August 1963."Includes bibliographical references.Mode of access: Internet

Water-landing characteristics of a 1/10-scale model of a winged missile /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Landing energy dissipation for manned reentry vehicles /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Includes bibliographical references.Mode of access: Internet

Effect of a load-alleviating structure on the landing behavior of a reentry-capsule model /

Hoffman, Edward L.
McGehee, John R.
Stubbs, Sandy M.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

Model investigation of the landing characteristics of a reentry spacecraft with a vertical-cylinder air bag for load alleviation /

McGehee, John R.
Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles; Space vehicles.Includes bibliogr...

Landing characteristics of a lentiucular-shaped reentry vehicle /

Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Major NASA subject terms:Space vehicles; Stresses and loads.Includes bi...

Water landing characteristics of a model of a winged reentry vehicle /

Stubbs, Sandy M.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 10.Mode of access: Internet

A concept of a manned satellite reentry which is completed with a glide landing /

Cheatham, Donald C.
United States. National Aeronautics and Space Administration.
Langley Research Center. Flight Research Division.

December 1959."Cover title.Includes bibliographical references (p. 25).Mode of access: Internet

Analytical investigation of the dynamic behavior of a nonlifting manned reentry vehicle. /

Lichtenstein, Jacob H.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Includes bibliographical references.Mode of access: Internet

Limited investigation of crushable structures for acceleration protection of occupants of vehicles at low impact speeds /

O'Bryan, Thomas C.
Hatch, Howard G.
United States. National Aeronautics and Space Administration.

Cover title."October 1959."Loads, landing, impact; Loads, landing, impact, land; Safety;Operating pr...

Hydrodynamic and aerodynamic characteristics of a model of a supersonic multijet water-based aircraft equipped with supercavitating hydrofoils /

McKann, Robert E.
Pearson, Albin O.
Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

A brief investigation of the effect of waves on the take-off resistance of a seaplane /

Mottard, Elmo J.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Hydrodynamic configurations, general; Hulls, seaplane, length-beam ratio...

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Experimental investigation of water-absorbent materials as possible heat sinks for hypersonic and reentry vehicles Robert P. Dengler and Reeves P. Cochran.

Dengler, Robert P.
Cochran, Reeves P.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Aircraft; Atmospheric entry; Fluid mechanics; Materials, other; Structures.I...

Landing-impact characteristics of load-alleviating struts on a model of a winged space vehicle /

Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Space vehicles; Stresses and loads.Includes bibliographical references.Mo...

Water landing impact accelerations for three models of reentry capsules /

Abstract

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Water landing impact accelerations for three models of reentry capsules /

Abstract

Extracted data

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