On the pitching and yawing motion of a spinning symmetric missile governed by an arbitrary nonlinear restoring moment /

Flight test of a pitch control for a spinning vehicle /

Garner, H. Douglas.
Reid, H. J. E.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

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

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

On the use of a magnetometer to determine the angular motion of a spinning body in regular precession /

Young, George R.
Timmons, Jesse D.
Langley Research Center.

Prepared at Langley Research Center."May 1964"--Cover.Includes bibliographical references (p. 13.Mod...

On the motion of a satellite in an asymmetrical gravitational field /

Musen, Peter, 1912-
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."January 1961."Cover title.Includes bibliographical referenc...

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Robinson, Ross B.
Foster, Gerald V.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Dynamics of tilting proprotor aircraft in cruise flight /

Johnson, Wayne, 1946-
U.S. Army Air Mobility Research and Development Laboratory.
Ames Research Center.

January 1974

Prepared at Ames Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes ...

Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies /

Williams, Kirby H.
James, Robert L., Jr.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 20)....

Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰ /

Hartman, Edward R.
Johnston, Patrick J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Gardiner, Robert A.
Zarovsky, Jacob.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"January 12, 1950."Includes bibliographical references (p. 12).Mode of access: Internet

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

Linear theory of impulsive velocity corrections for space mission guidance /

Cicolani, Luigi S.
Ames Research Center.

Prepared at Ames Research Center."April 1966"--Cover.Includes bibliographical references (p. 43).Mod...

Kinematic properties of the helicopter in coordinated turns /

Chen, Robert T. N.
Jeske, James A.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"Ames Research Center.""April 1981"--Cover.Includes bibliographical references.Mode of access: Inter...

The general motion of a variable-mass flexible rocket with internal flow /

Meirovich, Leonard.

"February 1970"--Cover.Includes bibliographical references.Prepared by the University of Cincinnati....

Flight test of a pitch control for a spinning vehicle /

Garner, H. Douglas.
Reid, H. J. E.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

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

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

On the use of a magnetometer to determine the angular motion of a spinning body in regular precession /

Young, George R.
Timmons, Jesse D.
Langley Research Center.

Prepared at Langley Research Center."May 1964"--Cover.Includes bibliographical references (p. 13.Mod...

On the motion of a satellite in an asymmetrical gravitational field /

Musen, Peter, 1912-
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."January 1961."Cover title.Includes bibliographical referenc...

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Robinson, Ross B.
Foster, Gerald V.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Dynamics of tilting proprotor aircraft in cruise flight /

Johnson, Wayne, 1946-
U.S. Army Air Mobility Research and Development Laboratory.
Ames Research Center.

January 1974

Prepared at Ames Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes ...

Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies /

Williams, Kirby H.
James, Robert L., Jr.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 20)....

Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰ /

Hartman, Edward R.
Johnston, Patrick J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Gardiner, Robert A.
Zarovsky, Jacob.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"January 12, 1950."Includes bibliographical references (p. 12).Mode of access: Internet

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

Linear theory of impulsive velocity corrections for space mission guidance /

Cicolani, Luigi S.
Ames Research Center.

Prepared at Ames Research Center."April 1966"--Cover.Includes bibliographical references (p. 43).Mod...

Kinematic properties of the helicopter in coordinated turns /

Chen, Robert T. N.
Jeske, James A.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"Ames Research Center.""April 1981"--Cover.Includes bibliographical references.Mode of access: Inter...

The general motion of a variable-mass flexible rocket with internal flow /

Meirovich, Leonard.

"February 1970"--Cover.Includes bibliographical references.Prepared by the University of Cincinnati....

Flight test of a pitch control for a spinning vehicle /

Garner, H. Douglas.
Reid, H. J. E.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

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

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

On the pitching and yawing motion of a spinning symmetric missile governed by an arbitrary nonlinear restoring moment /

Abstract

Extracted data

On the pitching and yawing motion of a spinning symmetric missile governed by an arbitrary nonlinear restoring moment /

Abstract

Extracted data

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