Qualification evaluation of the pitch control motor for the launch escape system of the Apollo spacecraft program /

Apollo experience report : aerothermodynamics evaluation /

Lee, Dorothy B.
Manned Spacecraft Center (U.S.)

January 1972

Prepared at the Manned Spacecraft Center, Houston, Tex.Cover title.Bibliography: p. 16.Mode of acces...

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...

The feasibility of a direct relay of Apollo spacecraft data via a communication satellite /

Schmid, P. E.
United States. National Aeronautics and Space Administration.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."August 1967"--Cover.Includes bibliographical references (p....

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. ...

Flight-test analysis of Apollo heat-shield material using the pacemaker vehicle system /

Graves, Randolph A., Jr.
Witte, William G.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 15-16).Mode of access: Internet

Apollo experience report : guidance and control systems /

Wilson, Raymond E.
United States. National Aeronautics and Space Administration.
Lyndon B. Johnson Space Center.

January 1976

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

Dynamic simulation of lunar module docking with Apollo command module in lunar orbit /

Hatch, Howard G.
Cobb, Jere B.
Pennington, Jack E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

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

Apollo experience report : descent propulsion system /

Hammock, William R.
Fisher, Arlie E.
Currie, Eldon C.
Manned Spacecraft Center (U.S.)

January 1973

Prepared at the Manned Spacecraft Center, Houston, Tex.Cover title.Bibliography: p. 31.Mode of acces...

Simulation of deployment dynamics of spinning spacecraft /

Lang, William E.
Honeycutt, George H.
Goddard Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1967."Includes bibliographical references (p. 20).Mode of access: Internet

Low-speed tests of an all-flexible parawing for landing a lifting-body spacecraft /

Bugg, Frank M.
Sleeman, William C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 12).Mode of access: Internet

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

Apollo experience report : guidance and control systems : digital autopilot design development /

Peters, William H.
Cox, Kenneth J.
Manned Spacecraft Center (U.S.)

January 1973

Prepared at the Manned Spacecraft Center, Houston, Tex.Cover title.Bibliography: p. 42.Mode of acces...

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. ...

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)....

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

Apollo experience report : aerothermodynamics evaluation /

Lee, Dorothy B.
Manned Spacecraft Center (U.S.)

January 1972

Prepared at the Manned Spacecraft Center, Houston, Tex.Cover title.Bibliography: p. 16.Mode of acces...

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...

The feasibility of a direct relay of Apollo spacecraft data via a communication satellite /

Schmid, P. E.
United States. National Aeronautics and Space Administration.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."August 1967"--Cover.Includes bibliographical references (p....

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. ...

Flight-test analysis of Apollo heat-shield material using the pacemaker vehicle system /

Graves, Randolph A., Jr.
Witte, William G.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 15-16).Mode of access: Internet

Apollo experience report : guidance and control systems /

Wilson, Raymond E.
United States. National Aeronautics and Space Administration.
Lyndon B. Johnson Space Center.

January 1976

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

Dynamic simulation of lunar module docking with Apollo command module in lunar orbit /

Hatch, Howard G.
Cobb, Jere B.
Pennington, Jack E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

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

Apollo experience report : descent propulsion system /

Hammock, William R.
Fisher, Arlie E.
Currie, Eldon C.
Manned Spacecraft Center (U.S.)

January 1973

Prepared at the Manned Spacecraft Center, Houston, Tex.Cover title.Bibliography: p. 31.Mode of acces...

Simulation of deployment dynamics of spinning spacecraft /

Lang, William E.
Honeycutt, George H.
Goddard Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1967."Includes bibliographical references (p. 20).Mode of access: Internet

Low-speed tests of an all-flexible parawing for landing a lifting-body spacecraft /

Bugg, Frank M.
Sleeman, William C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 12).Mode of access: Internet

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

Apollo experience report : guidance and control systems : digital autopilot design development /

Peters, William H.
Cox, Kenneth J.
Manned Spacecraft Center (U.S.)

January 1973

Prepared at the Manned Spacecraft Center, Houston, Tex.Cover title.Bibliography: p. 42.Mode of acces...

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. ...

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)....

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

Apollo experience report : aerothermodynamics evaluation /

Lee, Dorothy B.
Manned Spacecraft Center (U.S.)

January 1972

Prepared at the Manned Spacecraft Center, Houston, Tex.Cover title.Bibliography: p. 16.Mode of acces...

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...

The feasibility of a direct relay of Apollo spacecraft data via a communication satellite /

Schmid, P. E.
United States. National Aeronautics and Space Administration.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."August 1967"--Cover.Includes bibliographical references (p....

Qualification evaluation of the pitch control motor for the launch escape system of the Apollo spacecraft program /

Abstract

Extracted data

Qualification evaluation of the pitch control motor for the launch escape system of the Apollo spacecraft program /

Abstract

Extracted data

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