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

A study of a pilots ability to control during simulated stability augmentation system failures

Sadoff, Melvin.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

A preliminary study of handling-qualities requirements of supersonic transports in high-speed cruising flight using piloted simulators /

White, Maurice D.
United States. National Aeronautics and Space Administration.

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

Management of cryogenic propellants in a full-scale orbiting space vehicle /

Lacovic, Raymond F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 32).Mode of access: Internet

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

Orbital investigation of propellant dynamics in a large rocket booster /

Buchanan, H.J.
Bugg, F.M.
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 16).Mode of access: Internet

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...

Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63 /

Babb, C. Donald.
Fuller, Dennis E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 7).Mode of access: Internet

An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Levin, Alan D.
Smith, Ronald C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 18).Mode of access: Internet

Static stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20 /

Ferris, James C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Control of a large launch vehicle with limited thrust vectoring in the presence of winds /

Collins, Dennis F. (Dennis Francis), 1936-
Morgan, Homer G.
Langley Research Center.

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

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

Ware, George M.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Saturn V manual backup guidance and control piloted simulation study /

Kurkowski, Richard L.
Hardy, Gordon H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 26).Mode of access: Internet

Static stability characteristics of a series of hypersonic boost-glide configurations at mach numbers of 1.41 and 2.01 /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"November 1959."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Minimum energy reaction wheel control for a satellite scanning a small celestial area /

Wehrend, William R.
Bondi, Michael J.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Considerations of turbine cooling systems for Mach 3 flight /

Stepka, Francis S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 32).Mode of access: Internet

A study of a pilots ability to control during simulated stability augmentation system failures

Sadoff, Melvin.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

A preliminary study of handling-qualities requirements of supersonic transports in high-speed cruising flight using piloted simulators /

White, Maurice D.
United States. National Aeronautics and Space Administration.

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

Management of cryogenic propellants in a full-scale orbiting space vehicle /

Lacovic, Raymond F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 32).Mode of access: Internet

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

Orbital investigation of propellant dynamics in a large rocket booster /

Buchanan, H.J.
Bugg, F.M.
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 16).Mode of access: Internet

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...

Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63 /

Babb, C. Donald.
Fuller, Dennis E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 7).Mode of access: Internet

An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Levin, Alan D.
Smith, Ronald C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 18).Mode of access: Internet

Static stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20 /

Ferris, James C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Control of a large launch vehicle with limited thrust vectoring in the presence of winds /

Collins, Dennis F. (Dennis Francis), 1936-
Morgan, Homer G.
Langley Research Center.

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

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

Ware, George M.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Saturn V manual backup guidance and control piloted simulation study /

Kurkowski, Richard L.
Hardy, Gordon H.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 26).Mode of access: Internet

Static stability characteristics of a series of hypersonic boost-glide configurations at mach numbers of 1.41 and 2.01 /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"November 1959."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Minimum energy reaction wheel control for a satellite scanning a small celestial area /

Wehrend, William R.
Bondi, Michael J.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Considerations of turbine cooling systems for Mach 3 flight /

Stepka, Francis S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 32).Mode of access: Internet

A study of a pilots ability to control during simulated stability augmentation system failures

Sadoff, Melvin.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

A preliminary study of handling-qualities requirements of supersonic transports in high-speed cruising flight using piloted simulators /

White, Maurice D.
United States. National Aeronautics and Space Administration.

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

Management of cryogenic propellants in a full-scale orbiting space vehicle /

Lacovic, Raymond F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 32).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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