Flight control study of a manned re-entry vehicle /

Basic aerospace doctrine of the United States Air Force.

United States. Dept. of the Air Force.

Cover title."16 March 1984"--P. iii.Bibliography: p. B-1 -- B-5.Mode of access: Internet

Study of the use of a terminal controller technique for reentry guidance of a capsule-type vehicle /

Foudriat, Edwin C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Guidance and homing systems; Space vehicles; Stability and control.Includes b...

Inlet technology for air-launched missiles.

Zumpano, Francis R., author.
United Aircraft Corporation. Research Laboratories. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Volume II of Task I Interim Report, January 21, 1971 to September 20, 1971.""Project No. 3012, Task...

Telemetry transducer handbook.

Radiation Incorporated. compiler
United States. Wright Air Development Division. sponsor.
United States. Air Force. Air Research and Development Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.

"Project No. 4107, Task No. 82251.""28 April 1961."U.S. Air Force Contract No.Mode of access: Intern...

Study to determine aerodynamic characteristics on hypersonic re-entry configurations.

Malvestuto, Frank S., Jr., author.
Huggins, Vivan E., author.
Larrivee, Jules A. (Jules Alphonse), 1909-. author.
Mortzschky, Herbert A., author.
Marcy, William L., author.
Sullivan, Phillip J., author.
Lockheed Aircraft Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.

"Project No. 1366, Task No. 136608.""August 1962."Includes bibliographical references (pages 247-265...

Analytical investigation of the dynamic behavior of a nonlifting manned reentry vehicle. /

Lichtenstein, Jacob H.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Includes bibliographical references.Mode of access: Internet

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. ...

Investigation of the landing characteristics of a reentry vehicle having a canted multiple-air-bag load-alleviation system /

Stubbs, Sandy M.
McGehee, John R.
United States. National Aeronautics and Space Administration.

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

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

Hassell, James L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Measurement of thermal properties /

Fieldhouse, I. B., author.
Lang, J. I., author.
Armour Research Foundation (U.S.). sponsor.
United States. Wright Air Development Division. sponsor.
United States. Air Force. Air Research and Development Command. issuing body.

"July 1961.""Project No. 7381, Task No. 73812."U.S. Air Force Contract No.Mode of access: Internet

Development and flight test results of an autothrottle control system at Mach 3 cruise /

Gilyard, Glenn B.
Burken, John J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Hugh L. Dryden Flight Research Center.

January 1980

"July 1980"--Cover.Subject category 08."Dryden Flight Research Center."Mode of access: Internet

Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries /

Eggleston, John M. (John Marshall)
Cheatham, Donald C.
Baron, Sheldon.
Langley Research Center.

Prepared at Langley Research Center."April 1960."Cover title.Includes bibliographical references (p....

Releasable data on United States Air Force aerospace vehicles.

United States. Department of the Air Force.

1964 ed. published under title: Releasable data on USAF aerospace vehicles.Cover title: USAF aerospa...

Programmed text : flight controls, TH-55.

U.S. Army Aviation Center.

"Supersedes PT 2C011 0906 A, revised Mar 76.""February 1974."Mode of access: Internet

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

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

Basic aerospace doctrine of the United States Air Force.

United States. Dept. of the Air Force.

Cover title."16 March 1984"--P. iii.Bibliography: p. B-1 -- B-5.Mode of access: Internet

Study of the use of a terminal controller technique for reentry guidance of a capsule-type vehicle /

Foudriat, Edwin C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Guidance and homing systems; Space vehicles; Stability and control.Includes b...

Inlet technology for air-launched missiles.

Zumpano, Francis R., author.
United Aircraft Corporation. Research Laboratories. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Volume II of Task I Interim Report, January 21, 1971 to September 20, 1971.""Project No. 3012, Task...

Telemetry transducer handbook.

Radiation Incorporated. compiler
United States. Wright Air Development Division. sponsor.
United States. Air Force. Air Research and Development Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.

"Project No. 4107, Task No. 82251.""28 April 1961."U.S. Air Force Contract No.Mode of access: Intern...

Study to determine aerodynamic characteristics on hypersonic re-entry configurations.

Malvestuto, Frank S., Jr., author.
Huggins, Vivan E., author.
Larrivee, Jules A. (Jules Alphonse), 1909-. author.
Mortzschky, Herbert A., author.
Marcy, William L., author.
Sullivan, Phillip J., author.
Lockheed Aircraft Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.

"Project No. 1366, Task No. 136608.""August 1962."Includes bibliographical references (pages 247-265...

Analytical investigation of the dynamic behavior of a nonlifting manned reentry vehicle. /

Lichtenstein, Jacob H.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Includes bibliographical references.Mode of access: Internet

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. ...

Investigation of the landing characteristics of a reentry vehicle having a canted multiple-air-bag load-alleviation system /

Stubbs, Sandy M.
McGehee, John R.
United States. National Aeronautics and Space Administration.

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

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

Hassell, James L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Measurement of thermal properties /

Fieldhouse, I. B., author.
Lang, J. I., author.
Armour Research Foundation (U.S.). sponsor.
United States. Wright Air Development Division. sponsor.
United States. Air Force. Air Research and Development Command. issuing body.

"July 1961.""Project No. 7381, Task No. 73812."U.S. Air Force Contract No.Mode of access: Internet

Development and flight test results of an autothrottle control system at Mach 3 cruise /

Gilyard, Glenn B.
Burken, John J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Hugh L. Dryden Flight Research Center.

January 1980

"July 1980"--Cover.Subject category 08."Dryden Flight Research Center."Mode of access: Internet

Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries /

Eggleston, John M. (John Marshall)
Cheatham, Donald C.
Baron, Sheldon.
Langley Research Center.

Prepared at Langley Research Center."April 1960."Cover title.Includes bibliographical references (p....

Releasable data on United States Air Force aerospace vehicles.

United States. Department of the Air Force.

1964 ed. published under title: Releasable data on USAF aerospace vehicles.Cover title: USAF aerospa...

Programmed text : flight controls, TH-55.

U.S. Army Aviation Center.

"Supersedes PT 2C011 0906 A, revised Mar 76.""February 1974."Mode of access: Internet

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

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

Basic aerospace doctrine of the United States Air Force.

United States. Dept. of the Air Force.

Cover title."16 March 1984"--P. iii.Bibliography: p. B-1 -- B-5.Mode of access: Internet

Study of the use of a terminal controller technique for reentry guidance of a capsule-type vehicle /

Foudriat, Edwin C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Guidance and homing systems; Space vehicles; Stability and control.Includes b...

Inlet technology for air-launched missiles.

Zumpano, Francis R., author.
United Aircraft Corporation. Research Laboratories. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Volume II of Task I Interim Report, January 21, 1971 to September 20, 1971.""Project No. 3012, Task...

Flight control study of a manned re-entry vehicle /

Abstract

Extracted data

Flight control study of a manned re-entry vehicle /

Abstract

Extracted data

Related items

Related items