Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 5: Mach number 2 booster proximity data

Space Shuttle: MDAC/MMC space shuttle booster determination of stability and control characteristics and power effects at subsonic speed, Mach numbers zero and 0.26

Finch, C.
Roensch, R.
Lays, E.
Michna, D.

March 1971

Low speed wind tunnel tests of stability and control characteristics of space shuttle booster at sub...

Space shuttle: Static aerodynamic and control investigation of an expendable second stage with payload alone and with delta wing booster (B-15B-1)

Allen, E. C.
Eder, F. W.

June 1971

Aerodynamic force and moment coefficients for scale model of expendable second stage modified S-2 al...

Space shuttle: Determination of subsonic aerodynamic characteristics for McDonnell-Douglas generic high cross range shuttle orbiter

White, L. S.

March 1971

Low speed wind tunnel tests of subsonic aerodynamic properties of generic high cross range shuttle o...

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 1: Mach number 5 booster proximity data

Blackwell, K. L.
Decker, J. P.
Burt, R. H.
Trimmer, L. L.
Rampy, J. M.
Love, D. A.

July 1971

Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster pro...

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 2: Mach number 5 orbiter proximity data

Love, D. A.
Burt, R. H.
Blackwell, K. L.
Trimmer, L. L.
Decker, J. P.
Rampy, J. M.

July 1971

Space Shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0 Volume 4: Mach number 3 orbiter proximity data

Decker, J. P.
Rampy, J.
Love, D. A.
Trimmer, L. L.
Burt, R. H.
Blackwell, K. L.

August 1971

Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 3: Mach number 3 booster proximity data

Burt, R. H.
Decker, J. P.
Trimmer, L. L.
Love, D. A.
Blackwell, K. L.
Rampy, J. M.

August 1971

Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster pro...

Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 7: Proximity data at Mach 4 and 6, interference free and launch vehicle data

Love, D. A.
Decker, J. P.
Trimmer, L. L.
Strike, W. T.
Rampy, J. M.
Blackwell, K. L.

March 1972

Aerodynamic data obtained from a space shuttle abort stage separation wind tunnel test are presented...

Space shuttle: Effects of orbiter/booster proximity interference on the aerodynamic characteristics of the 0.0088105 scale MSC launch configuration, MSC test series S-28

February 1971

Supersonic phase of 0.0088105 scale MSC orbiter/booster test in four ft high speed wind tunne

Aerodynamic results of a separation effects test conducted in the AEDC 40 by 40 inch tunnel A facility on the Rockwell International launch configuration 3 (model 32-OTS) integrated vehicle (IA13), volume 2

Campbell, J. H., II

July 1975

Data figures are presented of the results of aerodynamic investigations conducted on the separation ...

Space shuttle: Determination of the aerodynamic interference between the space shuttle orbiter, external tank, and solid rocket booster on a 0.004 scale ascent configuration

Dehart, J.
Buchholz, R.
Ramsey, P. E.
Allen, E. C. JR.

April 1973

Wind tunnel tests were conducted to determine the aerodynamic interference between the space shuttle...

Space shuttle: Aerodynamic forces and moment on orbiter and booster during space shuttle abort separation

De Bevoise, J. M.

March 1971

Aerodynamic forces and moments on orbiter and booster during space shuttle abort separatio

Aerodynamic results of a separation effects test conducted in the AEDC 40 by 40 inch tunnel A facility on the Rockwell International launch configuration 3 (model 32-OTS) integrated vehicle (IA13), volume 3

Campbell, J. H., II

July 1975

Tabulated source data are presented of the results of aerodynamic investigations conducted on the se...

Aerodynamic results of a separation effects test conducted in the AEDC 40 by 40 inch tunnel A facility on the Rockwell International launch configuration 3 (model-OTS) integrated vehicle (IA13), volume 1

Campbell, J. H., II

July 1975

Experimental aerodynamic investigations were conducted from July 5 through July 17, 1973, on a 0.01 ...

Space shuttle: Low speed aerodynamic characteristics of the McDonnell Douglas space shuttle booster. Douglas Long Beach, low speed, wind tunnel test results

Finch, C. M.

December 1970

Low speed aerodynamic characteristics of McDonnell Douglas scale model space shuttle booste

Space Shuttle: MDAC/MMC space shuttle booster determination of stability and control characteristics and power effects at subsonic speed, Mach numbers zero and 0.26

Finch, C.
Roensch, R.
Lays, E.
Michna, D.

March 1971

Low speed wind tunnel tests of stability and control characteristics of space shuttle booster at sub...

Space shuttle: Static aerodynamic and control investigation of an expendable second stage with payload alone and with delta wing booster (B-15B-1)

Allen, E. C.
Eder, F. W.

June 1971

Aerodynamic force and moment coefficients for scale model of expendable second stage modified S-2 al...

Space shuttle: Determination of subsonic aerodynamic characteristics for McDonnell-Douglas generic high cross range shuttle orbiter

White, L. S.

March 1971

Low speed wind tunnel tests of subsonic aerodynamic properties of generic high cross range shuttle o...

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 1: Mach number 5 booster proximity data

Blackwell, K. L.
Decker, J. P.
Burt, R. H.
Trimmer, L. L.
Rampy, J. M.
Love, D. A.

July 1971

Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster pro...

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 2: Mach number 5 orbiter proximity data

Love, D. A.
Burt, R. H.
Blackwell, K. L.
Trimmer, L. L.
Decker, J. P.
Rampy, J. M.

July 1971

Space Shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0 Volume 4: Mach number 3 orbiter proximity data

Decker, J. P.
Rampy, J.
Love, D. A.
Trimmer, L. L.
Burt, R. H.
Blackwell, K. L.

August 1971

Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter pro...

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 3: Mach number 3 booster proximity data

Burt, R. H.
Decker, J. P.
Trimmer, L. L.
Love, D. A.
Blackwell, K. L.
Rampy, J. M.

August 1971

Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster pro...

Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 7: Proximity data at Mach 4 and 6, interference free and launch vehicle data

Love, D. A.
Decker, J. P.
Trimmer, L. L.
Strike, W. T.
Rampy, J. M.
Blackwell, K. L.

March 1972

Aerodynamic data obtained from a space shuttle abort stage separation wind tunnel test are presented...

Space shuttle: Effects of orbiter/booster proximity interference on the aerodynamic characteristics of the 0.0088105 scale MSC launch configuration, MSC test series S-28

February 1971

Supersonic phase of 0.0088105 scale MSC orbiter/booster test in four ft high speed wind tunne

Aerodynamic results of a separation effects test conducted in the AEDC 40 by 40 inch tunnel A facility on the Rockwell International launch configuration 3 (model 32-OTS) integrated vehicle (IA13), volume 2

Campbell, J. H., II

July 1975

Data figures are presented of the results of aerodynamic investigations conducted on the separation ...

Space shuttle: Determination of the aerodynamic interference between the space shuttle orbiter, external tank, and solid rocket booster on a 0.004 scale ascent configuration

Dehart, J.
Buchholz, R.
Ramsey, P. E.
Allen, E. C. JR.

April 1973

Wind tunnel tests were conducted to determine the aerodynamic interference between the space shuttle...

Space shuttle: Aerodynamic forces and moment on orbiter and booster during space shuttle abort separation

De Bevoise, J. M.

March 1971

Aerodynamic forces and moments on orbiter and booster during space shuttle abort separatio

Aerodynamic results of a separation effects test conducted in the AEDC 40 by 40 inch tunnel A facility on the Rockwell International launch configuration 3 (model 32-OTS) integrated vehicle (IA13), volume 3

Campbell, J. H., II

July 1975

Tabulated source data are presented of the results of aerodynamic investigations conducted on the se...

Aerodynamic results of a separation effects test conducted in the AEDC 40 by 40 inch tunnel A facility on the Rockwell International launch configuration 3 (model-OTS) integrated vehicle (IA13), volume 1

Campbell, J. H., II

July 1975

Experimental aerodynamic investigations were conducted from July 5 through July 17, 1973, on a 0.01 ...

Space shuttle: Low speed aerodynamic characteristics of the McDonnell Douglas space shuttle booster. Douglas Long Beach, low speed, wind tunnel test results

Finch, C. M.

December 1970

Low speed aerodynamic characteristics of McDonnell Douglas scale model space shuttle booste

Space Shuttle: MDAC/MMC space shuttle booster determination of stability and control characteristics and power effects at subsonic speed, Mach numbers zero and 0.26

Finch, C.
Roensch, R.
Lays, E.
Michna, D.

March 1971

Low speed wind tunnel tests of stability and control characteristics of space shuttle booster at sub...

Space shuttle: Static aerodynamic and control investigation of an expendable second stage with payload alone and with delta wing booster (B-15B-1)

Allen, E. C.
Eder, F. W.

June 1971

Aerodynamic force and moment coefficients for scale model of expendable second stage modified S-2 al...

Space shuttle: Determination of subsonic aerodynamic characteristics for McDonnell-Douglas generic high cross range shuttle orbiter

White, L. S.

March 1971

Low speed wind tunnel tests of subsonic aerodynamic properties of generic high cross range shuttle o...

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 5: Mach number 2 booster proximity data

Abstract

Extracted data

Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 5: Mach number 2 booster proximity data

Abstract

Extracted data

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