Entry aerodynamics at lunar return conditions obtained from the flight of Apollo 4 (AS-501)

Visual simulation facility for evaluation of lunar surface roving vehicles /

Vinz, Frank L.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."February 1968"--Cover.Includes bibliographical r...

Lunar landing and site selection study /

Lewis, James L.
Wheelwright, Charles D.
Manned Spacecraft Center (U.S.)

Prepared at Manned Spacecraft Center."September 1965"--Cover.Includes bibliographical references (p....

Minimum fuel ascent from the lunar surface /

Brown, Albert E.
Langley Research Center.

Prepared at Langley Research Center."September 1967"--Cover.Includes bibliographical references (p. ...

Return trajectories from the moon : some limits due to restrictions on entry range and landing lighting conditions /

Cicolani, Luigi S.
Ames Research Center.

Prepared at Ames Research Center."January 1964"--Cover.Includes bibliographical references (p. 13).M...

Aerodynamic stability characteristics of the Apollo launch escape vehicle (LEV) with canard surfaces deployed /

Moseley, William C.
Redd, Bass.
Manned Spacecraft Center (U.S.)

Prepared at Manned Spacecraft Center."December 1967"--Cover.Includes bibliographical references (p. ...

Dynamic model investigation of touchdown stability of lunar-landing vehicles /

Herr, Robert W.
Leonard, H. Wayne.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 22...

Full-scale dynamic landing-impact investigation of a prototype lunar module landing gear /

Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."March 1969"--Cover.Includes bibliographical references (p. 13)....

Wind-tunnel investigation of the aerodynamic pressures on the Apollo command module configuration /

Moseley, William C.
Wells, B. J.
United States. National Aeronautics and Space Administration.
Manned Spacecraft Center (U.S.)

Wind tunnel study of aerodynamic pressures on Apollo command module configuration.Prepared at the Ma...

Point return from a lunar mission for a vehicle that maneuvers within the earth's atmosphere /

Sommer, Simon C.
Short, Barbara J.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Atmospheric entry; Space mechanics.Includes bibliographical references.M...

Midcourse guidance for return from the moon to a geographically fixed landing site /

McLean, John D.
Cicolani, Luigi S.
Ames Research Center.

Prepared at Ames Research Center."March 1966"--Cover.Includes bibliographical references (p. 34).Mod...

Fixed-base visual simulation of pilot controlled descents of an advanced Apollo spacecraft with an all-flexible parawing /

Miller, G. Kimball.
Price, Douglas B. (Douglas Bailey), 1942-
Jacquet, Byron M.
Langley Research Center.

Prepared at Langley Research Center."March 1969"--Cover.Includes bibliographical references (p. 25)....

Effects of two probe antennas on aerodynamic characteristics of Apollo spacecraft at Mach 10.03 /

Putnam, Lawrence E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 6).Mode of access: Internet

A Flight evaluation of lunar landing trajectories using a jet VTOL test vehicle L. Stewart Rolls and Fred J. Drinkwater III.

Rolls, L. Stewart.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Major NASA subject terms:Includes bibliographical references.Mode of acc...

Mobility performance of the lunar roving vehicle : terrestrial studies, Apollo 15 results /

Costes, Nicholas C.
George, Edwin B.
Farmer, John E.
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration.

"December 1972."Cover title.Includes bibliographical references (p. 73-78).Mode of access: Internet

Some thrust and trajectory considerations for lunar landings /

Weber, Richard J.
Pauson, Werner M.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Space operations; Space sciences.Includes bibliographical references.Mod...

Visual simulation facility for evaluation of lunar surface roving vehicles /

Vinz, Frank L.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."February 1968"--Cover.Includes bibliographical r...

Lunar landing and site selection study /

Lewis, James L.
Wheelwright, Charles D.
Manned Spacecraft Center (U.S.)

Prepared at Manned Spacecraft Center."September 1965"--Cover.Includes bibliographical references (p....

Minimum fuel ascent from the lunar surface /

Brown, Albert E.
Langley Research Center.

Prepared at Langley Research Center."September 1967"--Cover.Includes bibliographical references (p. ...

Return trajectories from the moon : some limits due to restrictions on entry range and landing lighting conditions /

Cicolani, Luigi S.
Ames Research Center.

Prepared at Ames Research Center."January 1964"--Cover.Includes bibliographical references (p. 13).M...

Aerodynamic stability characteristics of the Apollo launch escape vehicle (LEV) with canard surfaces deployed /

Moseley, William C.
Redd, Bass.
Manned Spacecraft Center (U.S.)

Prepared at Manned Spacecraft Center."December 1967"--Cover.Includes bibliographical references (p. ...

Dynamic model investigation of touchdown stability of lunar-landing vehicles /

Herr, Robert W.
Leonard, H. Wayne.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 22...

Full-scale dynamic landing-impact investigation of a prototype lunar module landing gear /

Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."March 1969"--Cover.Includes bibliographical references (p. 13)....

Wind-tunnel investigation of the aerodynamic pressures on the Apollo command module configuration /

Moseley, William C.
Wells, B. J.
United States. National Aeronautics and Space Administration.
Manned Spacecraft Center (U.S.)

Wind tunnel study of aerodynamic pressures on Apollo command module configuration.Prepared at the Ma...

Point return from a lunar mission for a vehicle that maneuvers within the earth's atmosphere /

Sommer, Simon C.
Short, Barbara J.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Atmospheric entry; Space mechanics.Includes bibliographical references.M...

Midcourse guidance for return from the moon to a geographically fixed landing site /

McLean, John D.
Cicolani, Luigi S.
Ames Research Center.

Prepared at Ames Research Center."March 1966"--Cover.Includes bibliographical references (p. 34).Mod...

Fixed-base visual simulation of pilot controlled descents of an advanced Apollo spacecraft with an all-flexible parawing /

Miller, G. Kimball.
Price, Douglas B. (Douglas Bailey), 1942-
Jacquet, Byron M.
Langley Research Center.

Prepared at Langley Research Center."March 1969"--Cover.Includes bibliographical references (p. 25)....

Effects of two probe antennas on aerodynamic characteristics of Apollo spacecraft at Mach 10.03 /

Putnam, Lawrence E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 6).Mode of access: Internet

A Flight evaluation of lunar landing trajectories using a jet VTOL test vehicle L. Stewart Rolls and Fred J. Drinkwater III.

Rolls, L. Stewart.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Major NASA subject terms:Includes bibliographical references.Mode of acc...

Mobility performance of the lunar roving vehicle : terrestrial studies, Apollo 15 results /

Costes, Nicholas C.
George, Edwin B.
Farmer, John E.
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration.

"December 1972."Cover title.Includes bibliographical references (p. 73-78).Mode of access: Internet

Some thrust and trajectory considerations for lunar landings /

Weber, Richard J.
Pauson, Werner M.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Space operations; Space sciences.Includes bibliographical references.Mod...

Visual simulation facility for evaluation of lunar surface roving vehicles /

Vinz, Frank L.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."February 1968"--Cover.Includes bibliographical r...

Lunar landing and site selection study /

Lewis, James L.
Wheelwright, Charles D.
Manned Spacecraft Center (U.S.)

Prepared at Manned Spacecraft Center."September 1965"--Cover.Includes bibliographical references (p....

Minimum fuel ascent from the lunar surface /

Brown, Albert E.
Langley Research Center.

Prepared at Langley Research Center."September 1967"--Cover.Includes bibliographical references (p. ...

Entry aerodynamics at lunar return conditions obtained from the flight of Apollo 4 (AS-501)

Abstract

Extracted data

Entry aerodynamics at lunar return conditions obtained from the flight of Apollo 4 (AS-501)

Abstract

Extracted data

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