Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

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

Flight tests of a model having self-supporting fuel-carrying panels hinged to the wing tips /

Shanks, Robert E.
Grana, David C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 2, 1949."Includes bibliographical references (p. 6).Mode of access: Internet

Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid /

Morrell, Gerald joint author.
Humphrey, Jack C., joint author.
Sloop, John L., joint author.
Ladanyi, Dezso J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "July 19, 1950."Includes bibliographical references: p. 16.Mode of access: Internet

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

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

January 1951

"November 9, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation toward simplification of missile control systems /

Curfman, Howard J.
Crane, Harold L.
Strass, H. Kurt.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1953

"November 12, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies /

Williams, Kirby H.
James, Robert L., Jr.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 20)....

Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine /

Judd, Joseph H.
Trout, Otto F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

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 performance and description of a rocket vehicle for producing low-speed artificial meteors /

Brown, Clarence A.
Keating, Jean C.
Langley Research Center.

Prepared at Langley Research Center."April 1964"--Cover.Includes bibliographical references (p. 9).M...

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

Rainey, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1960

"March 7, 1951; Declassified July 28, 1960."Includes bibliographical references (p. 7).Mode of acces...

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

Performance charts for multistage rocket boosters /

MacKay, John S.
Weber, Richard J.
Lewis Research Center.

Prepared at Lewis Research Center."January 1961."Cover title.Includes bibliographical references (p....

Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40©� sweepback /

D'Aiutolo, Charles T.
Mason, Homer P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"October 31, 1950. Declassified September 17, 1958."Cover title.Includes bibliographical references ...

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

Flight tests of a model having self-supporting fuel-carrying panels hinged to the wing tips /

Shanks, Robert E.
Grana, David C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 2, 1949."Includes bibliographical references (p. 6).Mode of access: Internet

Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid /

Morrell, Gerald joint author.
Humphrey, Jack C., joint author.
Sloop, John L., joint author.
Ladanyi, Dezso J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "July 19, 1950."Includes bibliographical references: p. 16.Mode of access: Internet

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

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

January 1951

"November 9, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Investigation toward simplification of missile control systems /

Curfman, Howard J.
Crane, Harold L.
Strass, H. Kurt.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1953

"November 12, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studies /

Williams, Kirby H.
James, Robert L., Jr.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 20)....

Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine /

Judd, Joseph H.
Trout, Otto F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

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 performance and description of a rocket vehicle for producing low-speed artificial meteors /

Brown, Clarence A.
Keating, Jean C.
Langley Research Center.

Prepared at Langley Research Center."April 1964"--Cover.Includes bibliographical references (p. 9).M...

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

Rainey, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1960

"March 7, 1951; Declassified July 28, 1960."Includes bibliographical references (p. 7).Mode of acces...

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

Performance charts for multistage rocket boosters /

MacKay, John S.
Weber, Richard J.
Lewis Research Center.

Prepared at Lewis Research Center."January 1961."Cover title.Includes bibliographical references (p....

Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40©� sweepback /

D'Aiutolo, Charles T.
Mason, Homer P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"October 31, 1950. Declassified September 17, 1958."Cover title.Includes bibliographical references ...

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

Flight tests of a model having self-supporting fuel-carrying panels hinged to the wing tips /

Shanks, Robert E.
Grana, David C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 2, 1949."Includes bibliographical references (p. 6).Mode of access: Internet

Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid /

Morrell, Gerald joint author.
Humphrey, Jack C., joint author.
Sloop, John L., joint author.
Ladanyi, Dezso J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "July 19, 1950."Includes bibliographical references: p. 16.Mode of access: Internet

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Abstract

Extracted data

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Abstract

Extracted data

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