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

Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

"May 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Static longitudinal stability and performance of several ballistic spacecraft configuration in helium at a Mach number of 24.5 /

Johnston, Patrick J.
Snyder, Curtis D.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Satellites; Space vehicles; Sta...

Elements and parameters of the osculating orbit and their derivatives /

Dobson, Wilbur F.
Zimmerman, Arthur V.
Huff, Vearl N.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Space mechanics.Includes bibliographical references.Mode of access: Inter...

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 ...

Theory and design curves for a yo-yo de-spin mechanism for satellites /

Fedor, J. V.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Guidance and homing systems; Launching dynamics; Satellites; Stability and...

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

Grantham, William D.
United States. National Aeronautics and Space Administration.

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

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...

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...

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).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...

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...

An analytical approach to the design of an automatic discontinuous control system /

Taylor, Lawrence W.
Smith, John W.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Guidance and homing systems; Propulsion systems, liquid-fuel rockets; Propu...

Theory of artificial stabilization of missiles and space vehicles with exposition of four control principles /

Hoelker, Rudolf Franz
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Guidance and homing systems; Stability and control;Includes bibliographical ...

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 ...

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

Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

"May 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Static longitudinal stability and performance of several ballistic spacecraft configuration in helium at a Mach number of 24.5 /

Johnston, Patrick J.
Snyder, Curtis D.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Satellites; Space vehicles; Sta...

Elements and parameters of the osculating orbit and their derivatives /

Dobson, Wilbur F.
Zimmerman, Arthur V.
Huff, Vearl N.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Space mechanics.Includes bibliographical references.Mode of access: Inter...

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 ...

Theory and design curves for a yo-yo de-spin mechanism for satellites /

Fedor, J. V.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Guidance and homing systems; Launching dynamics; Satellites; Stability and...

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

Grantham, William D.
United States. National Aeronautics and Space Administration.

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

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...

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...

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).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...

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...

An analytical approach to the design of an automatic discontinuous control system /

Taylor, Lawrence W.
Smith, John W.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Guidance and homing systems; Propulsion systems, liquid-fuel rockets; Propu...

Theory of artificial stabilization of missiles and space vehicles with exposition of four control principles /

Hoelker, Rudolf Franz
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Guidance and homing systems; Stability and control;Includes bibliographical ...

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 ...

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

Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

"May 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Static longitudinal stability and performance of several ballistic spacecraft configuration in helium at a Mach number of 24.5 /

Johnston, Patrick J.
Snyder, Curtis D.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Satellites; Space vehicles; Sta...

Elements and parameters of the osculating orbit and their derivatives /

Dobson, Wilbur F.
Zimmerman, Arthur V.
Huff, Vearl N.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Space mechanics.Includes bibliographical references.Mode of access: Inter...

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

Abstract

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

Abstract

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