Effects of mass-loading variations and applied moments on motion and control of a manned rotating space vehicle. /

Effect of shield positioni and absorptivity on temperature distribution of a body shielded from solar radiation in space /

Nichols, Lester D.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Fluid mechanics; Materials, others; Propulsion system elements; Satellite...

Effect of inertia properties on attitude stability of nonrigid spin-stabilized spacecraft /

Lang, W. E.
Young, J. P.
Goddard Space Flight Center.

January 1974

Prepared at Goddard Space Flight Center.Cover title.Includes bibliographical references (p. 15-16).M...

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...

Study of systems using inertia wheels for precise attitude control of a satellite /

White, John S.
Hansen, Q. Marlon.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Satellites; Space vehicles; Stability and control.Includes bibliographical ...

Study of a satellite attitude control system using integrating gyros as torque sources /

White, John S.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Space mechanics; Satellites; Stability and control.Includes bibliograph...

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...

A Method of accurately reducing the spin rate of a rotating spacecraft /

Cornille, Henry J.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Launching dynamics; Navigation and navigation equipment; Satellites; Stab...

Experimental evaluation of the deceleration of aluminum cylinders rotating in a magnetic field and comments on magnetic damping of a flywheel control /

Eide, Donald G.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Satellites; Stability and control.Includes bibliographical references.Mode ...

Rotational Magnetodynamics and sterring of space vehicles /

Wilson, Raymond H.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Guidance and homing systems; Navigation and navigation equipment; Physi...

The effect of solar radiation pressure on the motion of an artificial satellite /

Bryant, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Astronomy; Astrophysics; Navigation and navigation equipment; Physics, ...

Equations of motion and design criteria for the despin of a vehicle by the radial release of weights and cables of finite mass /

Elde, Donald G.
Vaughan, Chester A.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Satellites; Stability and control;Includes bibliographical references.Mod...

Predicted performance of on-off systems for precise satellite attitude control /

Brown, Stuart C.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Satellites; Simulators and computers; Stability and control.Includes bibliog...

Influence of weight parameters on the propulsion requirements of orbit-launched vehicles y Dietrich W. Fellenz and Ronald J. Harris.

Fellenz, Dietrich W.
Harris, Ronald J.
United States. National Aeronautics and Space Administration.

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

Simulator studies of simple attitude control for spin-stabilized vehicles /

Garner, H. D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Simulators and computers; Stability and control.Includes bibliographica...

Simulation of deployment dynamics of spinning spacecraft /

Lang, William E.
Honeycutt, George H.
Goddard Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1967."Includes bibliographical references (p. 20).Mode of access: Internet

Effect of shield positioni and absorptivity on temperature distribution of a body shielded from solar radiation in space /

Nichols, Lester D.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Fluid mechanics; Materials, others; Propulsion system elements; Satellite...

Effect of inertia properties on attitude stability of nonrigid spin-stabilized spacecraft /

Lang, W. E.
Young, J. P.
Goddard Space Flight Center.

January 1974

Prepared at Goddard Space Flight Center.Cover title.Includes bibliographical references (p. 15-16).M...

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...

Study of systems using inertia wheels for precise attitude control of a satellite /

White, John S.
Hansen, Q. Marlon.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Satellites; Space vehicles; Stability and control.Includes bibliographical ...

Study of a satellite attitude control system using integrating gyros as torque sources /

White, John S.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Space mechanics; Satellites; Stability and control.Includes bibliograph...

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...

A Method of accurately reducing the spin rate of a rotating spacecraft /

Cornille, Henry J.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Launching dynamics; Navigation and navigation equipment; Satellites; Stab...

Experimental evaluation of the deceleration of aluminum cylinders rotating in a magnetic field and comments on magnetic damping of a flywheel control /

Eide, Donald G.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Satellites; Stability and control.Includes bibliographical references.Mode ...

Rotational Magnetodynamics and sterring of space vehicles /

Wilson, Raymond H.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Guidance and homing systems; Navigation and navigation equipment; Physi...

The effect of solar radiation pressure on the motion of an artificial satellite /

Bryant, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Astronomy; Astrophysics; Navigation and navigation equipment; Physics, ...

Equations of motion and design criteria for the despin of a vehicle by the radial release of weights and cables of finite mass /

Elde, Donald G.
Vaughan, Chester A.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Satellites; Stability and control;Includes bibliographical references.Mod...

Predicted performance of on-off systems for precise satellite attitude control /

Brown, Stuart C.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Satellites; Simulators and computers; Stability and control.Includes bibliog...

Influence of weight parameters on the propulsion requirements of orbit-launched vehicles y Dietrich W. Fellenz and Ronald J. Harris.

Fellenz, Dietrich W.
Harris, Ronald J.
United States. National Aeronautics and Space Administration.

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

Simulator studies of simple attitude control for spin-stabilized vehicles /

Garner, H. D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Simulators and computers; Stability and control.Includes bibliographica...

Simulation of deployment dynamics of spinning spacecraft /

Lang, William E.
Honeycutt, George H.
Goddard Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1967."Includes bibliographical references (p. 20).Mode of access: Internet

Effect of shield positioni and absorptivity on temperature distribution of a body shielded from solar radiation in space /

Nichols, Lester D.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Fluid mechanics; Materials, others; Propulsion system elements; Satellite...

Effect of inertia properties on attitude stability of nonrigid spin-stabilized spacecraft /

Lang, W. E.
Young, J. P.
Goddard Space Flight Center.

January 1974

Prepared at Goddard Space Flight Center.Cover title.Includes bibliographical references (p. 15-16).M...

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...

Effects of mass-loading variations and applied moments on motion and control of a manned rotating space vehicle. /

Abstract

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Effects of mass-loading variations and applied moments on motion and control of a manned rotating space vehicle. /

Abstract

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