Finite-thrust escape from and capture into circular and elliptic orbits /

A contribution to the theory of critical inclination of close earth satellites /

Aoki, Shinkō, 1927-
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."September 1963"--Cover.Includes bibliographical references ...

Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles /

Zurawski, Robert L.
Rapp, Douglas C.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 23).M...

Analysis of two thrusting techniques for soft lunar landings starting from a 50-mile altitude circular orbit /

Queijo, M. J.
Miller, G. Kimball.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Propulsion systems, theory; Space vehicles; Stability and control;Vehicle p...

Optimal finite-thrust transfer between planet-approach and departure asymptotes with specified intermediate orbit /

Willis, Edward A., Jr.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 56).Mode of access: Internet

A parametric study of constant thrust, electrically propelled Mars and Venus orbiting probes /

Rossa, Leonard G.

Prepared at Lewis Research Center."October 1964"--Cover.Includes bibliographical references (p. 28)....

Two-burn escape maneuvers with an intermediate coasting ellipse /

Willis, Edward A.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."February 1969"--Cover.Includes bibliographical references (p. 28)...

Low-thrust orbit raising in continuous sunlight /

Brown, Dennis W.
Lewis Research Center.

Prepared at Lewis Research Center."April 1964"--Cover.Includes bibliographical references (p. 16).Mo...

An analytical investigation of a simplified thrust-vector orientation technique for establishing lunar orbits /

Barker, L. Keith.
Sparrow, Gene W.
Langley Research Center.

Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 1...

The utilization of an impulsive solution in solving optimum trajectory problems with bounded thrust magnitude /

Jezewski, Donald J.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 27).Mode of access: Internet

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)...

A preliminary study of the use of finite-thrust engines for abort during launch of space vehicles /

McGowan, William A.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographi...

Starting conditions for nonoscillatory low-thrust planet-escape trajectories / Wilbur F. Dobson, John S. Mackay and Vearl N. Huff.

Dobson, Wilbur F.
Huff, Vearl N.
Mackay, John S.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Space mechanics.Includes bibliographical references.Mode of access: Intern...

Low-thrust orbit raising in continuous sunlight while thrusting in a plane perpendicular to the earth-sun line /

Ramler, James R.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 35).Mode of access: Internet

On the accuracy of an elliptical orbit determination /

Weirauch, Robert F.
Goddard Space Flight Center.

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

On the perturbations of small-eccentricity satellites /

Felsentreger, Theodore L.
United States. National Aeronautics and Space Administration.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."July 1968"--Cover.Includes bibliographical references (p. 2...

A contribution to the theory of critical inclination of close earth satellites /

Aoki, Shinkō, 1927-
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."September 1963"--Cover.Includes bibliographical references ...

Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles /

Zurawski, Robert L.
Rapp, Douglas C.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 23).M...

Analysis of two thrusting techniques for soft lunar landings starting from a 50-mile altitude circular orbit /

Queijo, M. J.
Miller, G. Kimball.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Propulsion systems, theory; Space vehicles; Stability and control;Vehicle p...

Optimal finite-thrust transfer between planet-approach and departure asymptotes with specified intermediate orbit /

Willis, Edward A., Jr.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 56).Mode of access: Internet

A parametric study of constant thrust, electrically propelled Mars and Venus orbiting probes /

Rossa, Leonard G.

Prepared at Lewis Research Center."October 1964"--Cover.Includes bibliographical references (p. 28)....

Two-burn escape maneuvers with an intermediate coasting ellipse /

Willis, Edward A.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."February 1969"--Cover.Includes bibliographical references (p. 28)...

Low-thrust orbit raising in continuous sunlight /

Brown, Dennis W.
Lewis Research Center.

Prepared at Lewis Research Center."April 1964"--Cover.Includes bibliographical references (p. 16).Mo...

An analytical investigation of a simplified thrust-vector orientation technique for establishing lunar orbits /

Barker, L. Keith.
Sparrow, Gene W.
Langley Research Center.

Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 1...

The utilization of an impulsive solution in solving optimum trajectory problems with bounded thrust magnitude /

Jezewski, Donald J.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 27).Mode of access: Internet

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)...

A preliminary study of the use of finite-thrust engines for abort during launch of space vehicles /

McGowan, William A.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Atmospheric entry; Space mechanics; Space vehicles.Includes bibliographi...

Starting conditions for nonoscillatory low-thrust planet-escape trajectories / Wilbur F. Dobson, John S. Mackay and Vearl N. Huff.

Dobson, Wilbur F.
Huff, Vearl N.
Mackay, John S.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Space mechanics.Includes bibliographical references.Mode of access: Intern...

Low-thrust orbit raising in continuous sunlight while thrusting in a plane perpendicular to the earth-sun line /

Ramler, James R.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 35).Mode of access: Internet

On the accuracy of an elliptical orbit determination /

Weirauch, Robert F.
Goddard Space Flight Center.

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

On the perturbations of small-eccentricity satellites /

Felsentreger, Theodore L.
United States. National Aeronautics and Space Administration.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."July 1968"--Cover.Includes bibliographical references (p. 2...

A contribution to the theory of critical inclination of close earth satellites /

Aoki, Shinkō, 1927-
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."September 1963"--Cover.Includes bibliographical references ...

Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles /

Zurawski, Robert L.
Rapp, Douglas C.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 23).M...

Analysis of two thrusting techniques for soft lunar landings starting from a 50-mile altitude circular orbit /

Queijo, M. J.
Miller, G. Kimball.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Propulsion systems, theory; Space vehicles; Stability and control;Vehicle p...

Finite-thrust escape from and capture into circular and elliptic orbits /

Abstract

Extracted data

Finite-thrust escape from and capture into circular and elliptic orbits /

Abstract

Extracted data

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