An Experimental and analytical investigation of the natural frequencies and mode shapes of a four-stage solid-propellant rocket vehicle / Sumner A. Leadbetter, Vernon L. Alley Jr., Robert W. Herr and A. Harper Gerringer.

An experimental investigation of the effect of high-pressure tailpipe length on the performance of solid-propellant motors for rocket-powered aircraft /

Rodriguez, Charles J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 24).Mode of access: Internet

An experimental technique for the investigation of tipoff forces associated with stage separation of multistage rocket vehicles /

Gungle, Robert L.
Leonard, H. Wayne.
Brosier, William S.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles;Launching dynamics; Missiles and ...

Investigation of the static longitudinal stability characteristics of a 0.067-scale model of a four-stage configuration of the Scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65 /

Jernell, Lloyd S.
Wong, Norman D.
Langley Research Center.

Prepared at Langley Research Center."Septmebr 1960."Cover title.Includes bibliographical references ...

Vibration and stability analysis of compressed rocket vehicles /

Glaser, Rudolf F.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."January 1965"--Cover.Includes bibliographical re...

An investigation of the natural frequencies and mode shapes of liquids in oblate spheroidal tanks /

Leonard, H. Wayne
Walton, William C.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Fluid mechanics; Launching facilities and operations; Launching dynamics; Ma...

A survey of structural dynamics of solid propellant rocket motors /

Baltrukonis, J. H.
Catholic University of America.
United States. National Aeronautics and Space Administration.

January 1966

"December 1966."Includes bibliographical references."Prepared under grant no.Mode of access: Interne...

An investigation of the response of a scaled model of a liquid-propellant multistage launch vehicle to longitudinal excitation /

Thompson, William M.
United States. National Aeronautics and Space Administration.

Cover title."May 1967."Includes bibliographical references (p. 23).Mode of access: Internet

Analytical and experimental studies of spherical solid-propellant rocket motors /

Thibodaux, Joseph G.
Wright, George.
Swain, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"August 16, 1957."Includes bibliographical references (p. 16).Mode of access: Internet

Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 /

Musial, Normal T.
Ward, James J.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Propulsion systems, liquid-fu...

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

Important research problems in missile and spacecraft structural dynamics : M.V. Barton.

Barton, Millard V. (Millard Vernon)
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

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

Measurements and analysis of solid-propellant-rocket vibrations obtained during a captive flight /

Schoenster, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

As part of an overall program to investigate the vibrational environment of small solid-propellant r...

Comparison of vibrations of a combination of solid-rocket launch vehicle and payload during a ground firing and launching /

Schoenster, James A.
Pierce, Harold B.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Vibration characteristics of 1/8-scale dynamic models of the space-shuttle solid-rocket boosters /

Leadbetter, Sumner A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 20-21).Mode of access: Internet

An experimental investigation of the effect of high-pressure tailpipe length on the performance of solid-propellant motors for rocket-powered aircraft /

Rodriguez, Charles J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 24).Mode of access: Internet

An experimental technique for the investigation of tipoff forces associated with stage separation of multistage rocket vehicles /

Gungle, Robert L.
Leonard, H. Wayne.
Brosier, William S.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles;Launching dynamics; Missiles and ...

Investigation of the static longitudinal stability characteristics of a 0.067-scale model of a four-stage configuration of the Scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65 /

Jernell, Lloyd S.
Wong, Norman D.
Langley Research Center.

Prepared at Langley Research Center."Septmebr 1960."Cover title.Includes bibliographical references ...

Vibration and stability analysis of compressed rocket vehicles /

Glaser, Rudolf F.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."January 1965"--Cover.Includes bibliographical re...

An investigation of the natural frequencies and mode shapes of liquids in oblate spheroidal tanks /

Leonard, H. Wayne
Walton, William C.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Fluid mechanics; Launching facilities and operations; Launching dynamics; Ma...

A survey of structural dynamics of solid propellant rocket motors /

Baltrukonis, J. H.
Catholic University of America.
United States. National Aeronautics and Space Administration.

January 1966

"December 1966."Includes bibliographical references."Prepared under grant no.Mode of access: Interne...

An investigation of the response of a scaled model of a liquid-propellant multistage launch vehicle to longitudinal excitation /

Thompson, William M.
United States. National Aeronautics and Space Administration.

Cover title."May 1967."Includes bibliographical references (p. 23).Mode of access: Internet

Analytical and experimental studies of spherical solid-propellant rocket motors /

Thibodaux, Joseph G.
Wright, George.
Swain, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"August 16, 1957."Includes bibliographical references (p. 16).Mode of access: Internet

Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 /

Musial, Normal T.
Ward, James J.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Propulsion systems, liquid-fu...

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

Important research problems in missile and spacecraft structural dynamics : M.V. Barton.

Barton, Millard V. (Millard Vernon)
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Stresses and loads; Structures.Includes bibliographical references.Mode of ac...

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

Measurements and analysis of solid-propellant-rocket vibrations obtained during a captive flight /

Schoenster, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

As part of an overall program to investigate the vibrational environment of small solid-propellant r...

Comparison of vibrations of a combination of solid-rocket launch vehicle and payload during a ground firing and launching /

Schoenster, James A.
Pierce, Harold B.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Vibration characteristics of 1/8-scale dynamic models of the space-shuttle solid-rocket boosters /

Leadbetter, Sumner A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 20-21).Mode of access: Internet

An experimental investigation of the effect of high-pressure tailpipe length on the performance of solid-propellant motors for rocket-powered aircraft /

Rodriguez, Charles J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 24).Mode of access: Internet

An experimental technique for the investigation of tipoff forces associated with stage separation of multistage rocket vehicles /

Gungle, Robert L.
Leonard, H. Wayne.
Brosier, William S.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles;Launching dynamics; Missiles and ...

Investigation of the static longitudinal stability characteristics of a 0.067-scale model of a four-stage configuration of the Scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65 /

Jernell, Lloyd S.
Wong, Norman D.
Langley Research Center.

Prepared at Langley Research Center."Septmebr 1960."Cover title.Includes bibliographical references ...

An Experimental and analytical investigation of the natural frequencies and mode shapes of a four-stage solid-propellant rocket vehicle / Sumner A. Leadbetter, Vernon L. Alley Jr., Robert W. Herr and A. Harper Gerringer.

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An Experimental and analytical investigation of the natural frequencies and mode shapes of a four-stage solid-propellant rocket vehicle / Sumner A. Leadbetter, Vernon L. Alley Jr., Robert W. Herr and A. Harper Gerringer.

Abstract

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