Optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints /

Approximate solutions to optimum climbing trajectory for a rocket-powered aircraft /

Miele, Angelo.
Cappellari, James O.
Purdue University.

Prepared at Purdue University."September 1959."Cover title.Includes bibliographical references (p. 3...

Simulation studies for planning an in-flight experiment to define manual guidance and control techniques for large launch vehicles /

Watson, DeLamar M.
Stinnett, Glen W.
Hardy, Gordon H.
Ames Research Center.

Prepared at Ames Research Center."April 1969"--Cover.Includes bibliographical references (p. 26).Mod...

Development of a method for optimal maneuver analysis of complex space missions /

McAdoo, Stewart F.
Dawkins, G. S. (George S.)
Jezewski, Donald J.
Lyndon B. Johnson Space Center.

January 1975

Prepared at the Johnson Space Center.Cover title.Includes bibliographical references (p. 25).Mode of...

Three-dimensional trajectory analysis for round-trip missions to Mars /

Knip, Gerald.
Zola, Charles L.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Launching facilities and operations; Launching dynamics; Space mechanics....

Analysis of maximum range trajectories for rocket-propelled lunar flying vehicles in a uniform gravitational field /

Childs, A. Gary.
Armstrong, Ernest S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."October 1969."Cover title.Includes bibliographical references (...

Optimal three-dimensional resusable tug trajectories for planetary missions including correction for nodal precession /

Borsody, Janos.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 34).Mode of ac...

Some numerical comparisons of three-body trajectories with patched two-body trajectories for low thrust rockets /

Strack, William C.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 24).Mode of access: Internet

Rendezvous capability of horizontal-take-off launch vehicle with air-breathing propulsion /

Jackson, Charlie M.
Langley Research Center.

Prepared at Langley Research Center."November 1964"--Cover.Includes bibliographical references (p. 2...

Performance capability of laser-powered launch vehicles using vertical ascent trajectories /

Spurlock, Omer F.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode of...

Low thrust space vehicle trajectory optimization using regularized variables /

Schwenzfeger, K. J.
George C. Marshall Space Flight Center.

January 1974

Prepared at George C. Marshall Space Flight Center.Cover title.Includes bibliographical references (...

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...

A trajectory code for maximizing the payload of multistage launch vehicles /

Spurlock, Omer F.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 166).Mode of access: Internet

Trajectories in the earth-moon space with symmetrical free return properties /

Schwaniger, Arthur J.
George C. Marshall Space Flight Center. Aeroballistics Division. Future Projects Branch.

Prepared at Marshall Space Flight Center's Future Projects Branch, Aeroballistics Division."June 196...

Characteristics of three precision circumlunar trajectories for the year 1968 /

Gapcynski, John P.
Woolston, Donald S.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Space mechanics.Includes bibliographical references.Mode of access: Interne...

Some requirements of electric and chemical thrust systems for space station drag cancellations /

Brown, Dennis W.
Lewis Research Center.

Prepared at Lewis Research Center."September 1964"--Cover.Includes bibliographical references (p. 7)...

Approximate solutions to optimum climbing trajectory for a rocket-powered aircraft /

Miele, Angelo.
Cappellari, James O.
Purdue University.

Prepared at Purdue University."September 1959."Cover title.Includes bibliographical references (p. 3...

Simulation studies for planning an in-flight experiment to define manual guidance and control techniques for large launch vehicles /

Watson, DeLamar M.
Stinnett, Glen W.
Hardy, Gordon H.
Ames Research Center.

Prepared at Ames Research Center."April 1969"--Cover.Includes bibliographical references (p. 26).Mod...

Development of a method for optimal maneuver analysis of complex space missions /

McAdoo, Stewart F.
Dawkins, G. S. (George S.)
Jezewski, Donald J.
Lyndon B. Johnson Space Center.

January 1975

Prepared at the Johnson Space Center.Cover title.Includes bibliographical references (p. 25).Mode of...

Three-dimensional trajectory analysis for round-trip missions to Mars /

Knip, Gerald.
Zola, Charles L.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Launching facilities and operations; Launching dynamics; Space mechanics....

Analysis of maximum range trajectories for rocket-propelled lunar flying vehicles in a uniform gravitational field /

Childs, A. Gary.
Armstrong, Ernest S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."October 1969."Cover title.Includes bibliographical references (...

Optimal three-dimensional resusable tug trajectories for planetary missions including correction for nodal precession /

Borsody, Janos.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 34).Mode of ac...

Some numerical comparisons of three-body trajectories with patched two-body trajectories for low thrust rockets /

Strack, William C.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 24).Mode of access: Internet

Rendezvous capability of horizontal-take-off launch vehicle with air-breathing propulsion /

Jackson, Charlie M.
Langley Research Center.

Prepared at Langley Research Center."November 1964"--Cover.Includes bibliographical references (p. 2...

Performance capability of laser-powered launch vehicles using vertical ascent trajectories /

Spurlock, Omer F.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode of...

Low thrust space vehicle trajectory optimization using regularized variables /

Schwenzfeger, K. J.
George C. Marshall Space Flight Center.

January 1974

Prepared at George C. Marshall Space Flight Center.Cover title.Includes bibliographical references (...

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...

A trajectory code for maximizing the payload of multistage launch vehicles /

Spurlock, Omer F.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 166).Mode of access: Internet

Trajectories in the earth-moon space with symmetrical free return properties /

Schwaniger, Arthur J.
George C. Marshall Space Flight Center. Aeroballistics Division. Future Projects Branch.

Prepared at Marshall Space Flight Center's Future Projects Branch, Aeroballistics Division."June 196...

Characteristics of three precision circumlunar trajectories for the year 1968 /

Gapcynski, John P.
Woolston, Donald S.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Space mechanics.Includes bibliographical references.Mode of access: Interne...

Some requirements of electric and chemical thrust systems for space station drag cancellations /

Brown, Dennis W.
Lewis Research Center.

Prepared at Lewis Research Center."September 1964"--Cover.Includes bibliographical references (p. 7)...

Approximate solutions to optimum climbing trajectory for a rocket-powered aircraft /

Miele, Angelo.
Cappellari, James O.
Purdue University.

Prepared at Purdue University."September 1959."Cover title.Includes bibliographical references (p. 3...

Simulation studies for planning an in-flight experiment to define manual guidance and control techniques for large launch vehicles /

Watson, DeLamar M.
Stinnett, Glen W.
Hardy, Gordon H.
Ames Research Center.

Prepared at Ames Research Center."April 1969"--Cover.Includes bibliographical references (p. 26).Mod...

Development of a method for optimal maneuver analysis of complex space missions /

McAdoo, Stewart F.
Dawkins, G. S. (George S.)
Jezewski, Donald J.
Lyndon B. Johnson Space Center.

January 1975

Prepared at the Johnson Space Center.Cover title.Includes bibliographical references (p. 25).Mode of...

Optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints /

Abstract

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Optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints /

Abstract

Extracted data

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