Analysis of two thrusting techniques for soft lunar landings starting from a 50-mile altitude circular orbit /

Point return from a lunar mission for a vehicle that maneuvers within the earth's atmosphere /

Sommer, Simon C.
Short, Barbara J.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Atmospheric entry; Space mechanics.Includes bibliographical references.M...

Analysis of maximum range trajectories for rocket-propelled lunar flying vehicles in a uniform gravitational field /

Childs, A. Gary.
Armstrong, Ernest S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."October 1969."Cover title.Includes bibliographical references (...

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...

Some thrust and trajectory considerations for lunar landings /

Weber, Richard J.
Pauson, Werner M.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Space operations; Space sciences.Includes bibliographical references.Mod...

A technique for thrust-vector orientation during manual control of lunar landings from a synchronous orbit /

Barker, L. Keith.
Queijo, M. J.
Langley Research Center.

Prepared at Langley Research Center."June 1964"--Cover.Includes bibliographical references (p. 11).M...

An analytical investigation of a simplified thrust-vector orientation technique for establishing lunar orbits /

Barker, L. Keith.
Sparrow, Gene W.
Langley Research Center.

Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 1...

A preliminary study of the orbits of merit for moon probes / Su-Shu Huang.

Huang, Su-Shu, 1915-
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Launching dynamics; Missiles and satellite carriers; Space mechanics.Include...

A study of thrust vector steering for rendezvous with a near-earth satellite utilizing a three-stage vehicle launched out of the satellite plane /

Llewellyn, Charles P.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Guidance and homing; Launching dynamics; Space mechanics; Satellites; Sta...

Interaction of highly underexpanded jets with simulated lunar surfaces /

Stitt, Leonard E.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicl...

Lunar trajectories /

Weber, Richard J.
Burley, Richard R.
Pauson, Werner M.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Guidance and homing systems; Launching dynamics; Navigation and navigation...

Analysis of self-locomotive performance of lunar explorers based on experimental reduced-gravity studies /

Hewes, Donald E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 19).Mode of access: Internet

A Flight evaluation of lunar landing trajectories using a jet VTOL test vehicle L. Stewart Rolls and Fred J. Drinkwater III.

Rolls, L. Stewart.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Major NASA subject terms:Includes bibliographical references.Mode of acc...

Fixed-base-simulator study of the ability of a pilot to perform soft lunar landings /

Queijo, M. J.
Fletcher, Herman S.
Miller, G. Kimball.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Piloting.Includes bibliographical references.Mode of access: Internet

A preliminary study of the use of finite-thrust engines for abort during launch of space vehicles /

McGowan, William A.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographi...

The influence of precession of Earth rendezvous orbits on lunar mission requirements

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

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Point return from a lunar mission for a vehicle that maneuvers within the earth's atmosphere /

Sommer, Simon C.
Short, Barbara J.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Atmospheric entry; Space mechanics.Includes bibliographical references.M...

Analysis of maximum range trajectories for rocket-propelled lunar flying vehicles in a uniform gravitational field /

Childs, A. Gary.
Armstrong, Ernest S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."October 1969."Cover title.Includes bibliographical references (...

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...

Some thrust and trajectory considerations for lunar landings /

Weber, Richard J.
Pauson, Werner M.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Space operations; Space sciences.Includes bibliographical references.Mod...

A technique for thrust-vector orientation during manual control of lunar landings from a synchronous orbit /

Barker, L. Keith.
Queijo, M. J.
Langley Research Center.

Prepared at Langley Research Center."June 1964"--Cover.Includes bibliographical references (p. 11).M...

An analytical investigation of a simplified thrust-vector orientation technique for establishing lunar orbits /

Barker, L. Keith.
Sparrow, Gene W.
Langley Research Center.

Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 1...

A preliminary study of the orbits of merit for moon probes / Su-Shu Huang.

Huang, Su-Shu, 1915-
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Launching dynamics; Missiles and satellite carriers; Space mechanics.Include...

A study of thrust vector steering for rendezvous with a near-earth satellite utilizing a three-stage vehicle launched out of the satellite plane /

Llewellyn, Charles P.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Guidance and homing; Launching dynamics; Space mechanics; Satellites; Sta...

Interaction of highly underexpanded jets with simulated lunar surfaces /

Stitt, Leonard E.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicl...

Lunar trajectories /

Weber, Richard J.
Burley, Richard R.
Pauson, Werner M.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Guidance and homing systems; Launching dynamics; Navigation and navigation...

Analysis of self-locomotive performance of lunar explorers based on experimental reduced-gravity studies /

Hewes, Donald E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 19).Mode of access: Internet

A Flight evaluation of lunar landing trajectories using a jet VTOL test vehicle L. Stewart Rolls and Fred J. Drinkwater III.

Rolls, L. Stewart.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Major NASA subject terms:Includes bibliographical references.Mode of acc...

Fixed-base-simulator study of the ability of a pilot to perform soft lunar landings /

Queijo, M. J.
Fletcher, Herman S.
Miller, G. Kimball.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Piloting.Includes bibliographical references.Mode of access: Internet

A preliminary study of the use of finite-thrust engines for abort during launch of space vehicles /

McGowan, William A.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographi...

The influence of precession of Earth rendezvous orbits on lunar mission requirements

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

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Point return from a lunar mission for a vehicle that maneuvers within the earth's atmosphere /

Sommer, Simon C.
Short, Barbara J.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Atmospheric entry; Space mechanics.Includes bibliographical references.M...

Analysis of maximum range trajectories for rocket-propelled lunar flying vehicles in a uniform gravitational field /

Childs, A. Gary.
Armstrong, Ernest S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."October 1969."Cover title.Includes bibliographical references (...

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...

Analysis of two thrusting techniques for soft lunar landings starting from a 50-mile altitude circular orbit /

Abstract

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Analysis of two thrusting techniques for soft lunar landings starting from a 50-mile altitude circular orbit /

Abstract

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