Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 11

Results of tests OA26 and IA16 in the NASA/ARC 3.5-foot hypersonic wind tunnel on an 0.015-scale model (36-OTS) of the space shuttle configuration 140A/B to obtain pressures for venting analysis

Thornton, D. E.
Spangler, R. H.
Polek, T. E.

April 1974

Tests were conducted, from November 15 to December 4, 1973, to obtain surface pressure data on an 0....

Investigations of the 0.020-scale 88-OTS Integrated Space Shuttle Vehicle Jet-Plume Model in the NASA/Ames Research Center 11 by 11-Foot Unitary Plan Wind Tunnel (IA80)

Nichols, M. E.

September 1976

Tabulated pressure data are presented for the external tank and the external tank base. For abstract...

An investigation in the NASA MSFC 14-inch trisonic wind tunnel to determine the pressure distribution over the components of a 0.004 scale version of the Rockwell MCR 0074 baseline shuttle ascent configuration (IA32F), volume 1

Ramsey, P. E.

September 1975

Data were obtained for Mach numbers from 0.6 to 3.48, angles of attack from -10 to 10 degrees, and a...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 9

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the external tank and the SRM nozzle of the space shu...

Airloads investigation of an 0.30-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 5

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the lower wing surface of the space shuttle launch ve...

Airloads investigation of an 0.030-scale model of the Space Shuttle Vehicle 140 A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for MACH range 0.6 to 1.4 (IA14A), volume 10

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the external tank base and SRM booster base of the sp...

Airloads investigation of an 0.030 scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 7

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the left and right vertical tail surface of the space...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the arc 11-foot unitary plan wind tunnel for Mach range 0.6 to 1.4 (IA14A), Volume 2

Gillins, R. L.

March 1975

Results of tests conducted on an 0.030-scale launch configuration model of the space shuttle vehicle...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the arc 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 8

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the SRM booster of the space shuttle launch vehicle c...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the arc 11-foot unitary plan wind tunnel for Mach range 0.6 to 1.4 (IA14A), volume 1

Gillins, R. L.

February 1975

The results of the tests are presented along with aerodynamic loads data obtained at Mach numbers fr...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 6

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the upper wing surface of the space shuttle launch ve...

Investigations on an 0.030-scale space shuttle vehicle configuration 140A/B orbiter model in the Ames Research Center 9 by 7-foot supersonic wind tunnel (OA53B)

Nichols, M. E.

July 1974

A wind tunnel test of an 0.030-scale space shuttle vehicle orbiter configuration 140A/B model was co...

Results of a pressure loads investigation on a 0.030-scale model (47-OTS) of the integrated space shuttle vehicle configuration 5 in the NASA Ames Research Center 9 by 7 foot leg of the unitary plan wind tunnel (IA81B), volume 1

Chee, E.

October 1975

The investigations of pressure distributions are presented for aeroloads analysis at Mach numbers fr...

Results of investigations conducted in the LaRC 4-foot unitary plan wind tunnel leg no. 1 using the 0.010-scale 72-OTS model of the space shuttle integrated vehicle (IA94A)

Nichols, M. E.

December 1976

Aero-loads investigations were conducted on the updated configuration-5 space shuttle launch vehicle...

Aeroheating (pressure) characteristics on a 0.10-scale version of the vehicle 3 space shuttle configuration (26-OTS) in the Langley Research Center 4-foot wind tunnel (IH4)

Kingsland, R. B.

May 1976

Results of wind tunnel tests, conducted at the Langley Research Center Unitary Plan Wind Tunnel, are...

Results of tests OA26 and IA16 in the NASA/ARC 3.5-foot hypersonic wind tunnel on an 0.015-scale model (36-OTS) of the space shuttle configuration 140A/B to obtain pressures for venting analysis

Thornton, D. E.
Spangler, R. H.
Polek, T. E.

April 1974

Tests were conducted, from November 15 to December 4, 1973, to obtain surface pressure data on an 0....

Investigations of the 0.020-scale 88-OTS Integrated Space Shuttle Vehicle Jet-Plume Model in the NASA/Ames Research Center 11 by 11-Foot Unitary Plan Wind Tunnel (IA80)

Nichols, M. E.

September 1976

Tabulated pressure data are presented for the external tank and the external tank base. For abstract...

An investigation in the NASA MSFC 14-inch trisonic wind tunnel to determine the pressure distribution over the components of a 0.004 scale version of the Rockwell MCR 0074 baseline shuttle ascent configuration (IA32F), volume 1

Ramsey, P. E.

September 1975

Data were obtained for Mach numbers from 0.6 to 3.48, angles of attack from -10 to 10 degrees, and a...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 9

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the external tank and the SRM nozzle of the space shu...

Airloads investigation of an 0.30-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 5

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the lower wing surface of the space shuttle launch ve...

Airloads investigation of an 0.030-scale model of the Space Shuttle Vehicle 140 A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for MACH range 0.6 to 1.4 (IA14A), volume 10

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the external tank base and SRM booster base of the sp...

Airloads investigation of an 0.030 scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 7

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the left and right vertical tail surface of the space...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the arc 11-foot unitary plan wind tunnel for Mach range 0.6 to 1.4 (IA14A), Volume 2

Gillins, R. L.

March 1975

Results of tests conducted on an 0.030-scale launch configuration model of the space shuttle vehicle...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the arc 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 8

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the SRM booster of the space shuttle launch vehicle c...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the arc 11-foot unitary plan wind tunnel for Mach range 0.6 to 1.4 (IA14A), volume 1

Gillins, R. L.

February 1975

The results of the tests are presented along with aerodynamic loads data obtained at Mach numbers fr...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 6

Gillins, R. L.

March 1975

Pressure data are presented in tabular form on the upper wing surface of the space shuttle launch ve...

Investigations on an 0.030-scale space shuttle vehicle configuration 140A/B orbiter model in the Ames Research Center 9 by 7-foot supersonic wind tunnel (OA53B)

Nichols, M. E.

July 1974

A wind tunnel test of an 0.030-scale space shuttle vehicle orbiter configuration 140A/B model was co...

Results of a pressure loads investigation on a 0.030-scale model (47-OTS) of the integrated space shuttle vehicle configuration 5 in the NASA Ames Research Center 9 by 7 foot leg of the unitary plan wind tunnel (IA81B), volume 1

Chee, E.

October 1975

The investigations of pressure distributions are presented for aeroloads analysis at Mach numbers fr...

Results of investigations conducted in the LaRC 4-foot unitary plan wind tunnel leg no. 1 using the 0.010-scale 72-OTS model of the space shuttle integrated vehicle (IA94A)

Nichols, M. E.

December 1976

Aero-loads investigations were conducted on the updated configuration-5 space shuttle launch vehicle...

Aeroheating (pressure) characteristics on a 0.10-scale version of the vehicle 3 space shuttle configuration (26-OTS) in the Langley Research Center 4-foot wind tunnel (IH4)

Kingsland, R. B.

May 1976

Results of wind tunnel tests, conducted at the Langley Research Center Unitary Plan Wind Tunnel, are...

Results of tests OA26 and IA16 in the NASA/ARC 3.5-foot hypersonic wind tunnel on an 0.015-scale model (36-OTS) of the space shuttle configuration 140A/B to obtain pressures for venting analysis

Thornton, D. E.
Spangler, R. H.
Polek, T. E.

April 1974

Tests were conducted, from November 15 to December 4, 1973, to obtain surface pressure data on an 0....

Investigations of the 0.020-scale 88-OTS Integrated Space Shuttle Vehicle Jet-Plume Model in the NASA/Ames Research Center 11 by 11-Foot Unitary Plan Wind Tunnel (IA80)

Nichols, M. E.

September 1976

Tabulated pressure data are presented for the external tank and the external tank base. For abstract...

An investigation in the NASA MSFC 14-inch trisonic wind tunnel to determine the pressure distribution over the components of a 0.004 scale version of the Rockwell MCR 0074 baseline shuttle ascent configuration (IA32F), volume 1

Ramsey, P. E.

September 1975

Data were obtained for Mach numbers from 0.6 to 3.48, angles of attack from -10 to 10 degrees, and a...

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 11

Abstract

Extracted data

Airloads investigation of an 0.030-scale model of the space shuttle vehicle 140A/B launch configuration (model 47-OTS) in the ARC 11-foot Unitary Plan Wind Tunnel for Mach range 0.6 to 1.4 (IA14A), volume 11

Abstract

Extracted data

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