The effect of lateral- and longitudinal-range control on allowable entry conditions for a point return from space /

Piloted simulator tests of a guidance system which can continuously predict landing point of a low L/D vehicle during atmosphere re-entry /

Wingrove, Rodney C.
Coate, Robert E.
United States. National Aeronautics and Space Administration.

Cover title." March 1961."Atmospheric entry; Navigation and navigation equipment; Piloting; Space ve...

Development of satisfactory lateral-directional handling qualities in the landing approach /

Stapleford, Robert L.
Systems Technology, inc.
United States. National Aeronautics and Space Administration.

January 1965

"July 1965." --- title page.Bibliography: p. 82-83.Prepared by Systems Technology, Inc., Hawthorne, ...

Effects of flight conditions at booster separation on payload weight in orbit /

Nelson, Richard D.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Missiles and satellite carriers; Space mechanics.Includes bibliographica...

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...

An analytical method for studying the lateral motion of atmosphere entry vehicles. /

Slye, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Atmospheric entry; Guidance and homing systems; Navigation and navigati...

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...

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

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

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

Effects of some typical geometrical constraints on lunar trajectories /

Tolson, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Space mechanics; Space vehicles.Includes bibliog...

Return trajectories from the moon : some limits due to restrictions on entry range and landing lighting conditions /

Cicolani, Luigi S.
Ames Research Center.

Prepared at Ames Research Center."January 1964"--Cover.Includes bibliographical references (p. 13).M...

Effects of control-feel configuration on airplane longitudinal control response /

Crane, Harold L.
Sommers, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control; ...

Trajectory control in rendezvous problems using proportional navigation /

Cocilani, Luigi S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Space mechanics; Satellites; Space vehicles.Includes bibliographical refere...

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...

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...

A study of the optimum velocity change to intercept and rendezvous /

Eggleston, John M.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Guidance and homing systems; Space mechanics; Satellites.Includes biblio...

Feasibility study of a circumlunar photographic experiment /

Michael, William H.
Gapcynski, John P.
Tolson, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographical r...

Piloted simulator tests of a guidance system which can continuously predict landing point of a low L/D vehicle during atmosphere re-entry /

Wingrove, Rodney C.
Coate, Robert E.
United States. National Aeronautics and Space Administration.

Cover title." March 1961."Atmospheric entry; Navigation and navigation equipment; Piloting; Space ve...

Development of satisfactory lateral-directional handling qualities in the landing approach /

Stapleford, Robert L.
Systems Technology, inc.
United States. National Aeronautics and Space Administration.

January 1965

"July 1965." --- title page.Bibliography: p. 82-83.Prepared by Systems Technology, Inc., Hawthorne, ...

Effects of flight conditions at booster separation on payload weight in orbit /

Nelson, Richard D.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Missiles and satellite carriers; Space mechanics.Includes bibliographica...

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...

An analytical method for studying the lateral motion of atmosphere entry vehicles. /

Slye, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Atmospheric entry; Guidance and homing systems; Navigation and navigati...

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...

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

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

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

Effects of some typical geometrical constraints on lunar trajectories /

Tolson, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Space mechanics; Space vehicles.Includes bibliog...

Return trajectories from the moon : some limits due to restrictions on entry range and landing lighting conditions /

Cicolani, Luigi S.
Ames Research Center.

Prepared at Ames Research Center."January 1964"--Cover.Includes bibliographical references (p. 13).M...

Effects of control-feel configuration on airplane longitudinal control response /

Crane, Harold L.
Sommers, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control; ...

Trajectory control in rendezvous problems using proportional navigation /

Cocilani, Luigi S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Space mechanics; Satellites; Space vehicles.Includes bibliographical refere...

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...

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...

A study of the optimum velocity change to intercept and rendezvous /

Eggleston, John M.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Guidance and homing systems; Space mechanics; Satellites.Includes biblio...

Feasibility study of a circumlunar photographic experiment /

Michael, William H.
Gapcynski, John P.
Tolson, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographical r...

Piloted simulator tests of a guidance system which can continuously predict landing point of a low L/D vehicle during atmosphere re-entry /

Wingrove, Rodney C.
Coate, Robert E.
United States. National Aeronautics and Space Administration.

Cover title." March 1961."Atmospheric entry; Navigation and navigation equipment; Piloting; Space ve...

Development of satisfactory lateral-directional handling qualities in the landing approach /

Stapleford, Robert L.
Systems Technology, inc.
United States. National Aeronautics and Space Administration.

January 1965

"July 1965." --- title page.Bibliography: p. 82-83.Prepared by Systems Technology, Inc., Hawthorne, ...

Effects of flight conditions at booster separation on payload weight in orbit /

Nelson, Richard D.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Missiles and satellite carriers; Space mechanics.Includes bibliographica...

The effect of lateral- and longitudinal-range control on allowable entry conditions for a point return from space /

Abstract

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The effect of lateral- and longitudinal-range control on allowable entry conditions for a point return from space /

Abstract

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