Transonic control effectiveness for full and partial span elevon configurations on a 0.0165 scale model space shuttle orbiter tested in the LaRC 8-foot transonic wind tunnel (LA48)

Wind tunnel test of the 0.010-scale space shuttle integrated vehicle in the NASA-Ames 3.5 foot hypersonic wind tunnel (IA10)

Fitzgerald, F. F.
Mellenthin, J. A.
Cleary, J. W.
Petrozzi, M. T.

December 1973

Experimental aerodynamic investigations were conducted in the NASA Ames Research Center 3.5-Foot Hyp...

Results of transonic tests in the NASA/MSFC 14-inch trisonic wind tunnel on a 0.004-scale model (74-OTS) space shuttle launch vehicle (FA25)

Lundy, T. E.

January 1979

The primary objective of the test was to determine the aerodynamic increments due to the attach stru...

Results of investigations on an 0.015-scale configuration 140A/B space shuttle vehicle orbiter model (49-0) in the NASA/Langley Research Center 8-foot transonic pressure tunnel (OA25)

Nichols, M. E.

February 1974

Aerodynamic force and moment tests were conducted on an 0.015-scale space shuttle vehicle configurat...

Supersonic control effectiveness for full and partial span elevon configurations on a 0.0165 scale model space shuttle orbiter tested in the LaRC unitary plan wind tunnel (LA49)

March 1977

A wind tunnel test is reported on an early version of the space shuttle orbiter (designated 089B-139...

Results of transonic wind tunnel tests on an 0.010-scale space shuttle mated vehicle model 72-OTS in the LaRC 8-foot TPT (IA43)

Milam, M. D.
Petrozzi, M. T.

April 1975

Experimental aerodynamic investigations were conducted in NASA/Langley 8-Foot transonic pressure tun...

Investigations on an 0.030-scale space shuttle vehicle configuration 140A/B orbiter model in the Ames Research Center unitary plan 8 by 7-foot supersonic wind tunnel (0A53C)

Nichols, M. E.

July 1974

A wind tunnel test was conducted of an 0.030 scale model of the space shuttle orbiter in a supersoni...

Subsonic and transonic aerodynamic characteristics associated with variations in the geometry of the forward portion of irregular planform wings on a .01875 scale LO-100 Langley concept space shuttle orbiter in the Langley 8 foot TPT (LA7B)

Vaughn, J. E.
Poucher, D. E.

March 1973

The experimental longitudinal-and lateral-directional stability characteristics of a Langley concept...

Wind tunnel tests of an 0.015-scale configuration 140A/B space shuttle orbiter model (67-0) in the NASA/LRC 8-foot TPT to obtain transonic aerodynamic force data (OA106)

Burrows, R. R.

October 1974

These tests were conducted to obtain longitudinal stability and control data for Mach numbers from 0...

Terminal area energy management regime investigations utilizing an 0.030-scale model (47-0) of the space shuttle vehicle orbiter configuration 140A/B/C/R in the Ames Research Center 11 x 11 foot transonic wind tunnel (OH/48)

Hawthorne, P. J.

July 1976

Data obtained in a wind tunnel test were examined to: (1) obtain pressure distributions, forces and ...

Wind tunnel tests of the 0.010-scale space shuttle integrated vehicle (model 52-QT) in the NASA/Ames 3.5-foot hypersonic wind tunnel (IA18)

Stone, J.
Chee, E.
Mellenthin, J. A.
Esparza, V.

March 1975

Experimental aerodynamic investigations were conducted in the NASA/Ames Research Center 3.5-foot hyp...

Results of investigations on an 0.015 scale 140A/B configuration space shuttle vehicle orbiter model (49-0) in the LTV 4 by 4-foot high speed wind tunnel (0A84)

Esparza, V.
Embury, W. R.

August 1974

Data obtained from a wind tunnel test of an 0.015-scale 140 A/B configuration space shuttle vehicle ...

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...

Subsonic, transonic, and supersonic stability and control characteristics of the -147B space shuttle orbiter

Mennell, R. C.

October 1973

Experimental aerodynamic investigations were conducted on 0.015 scale representations of two Space S...

Results of investigations on a 0.015-scale model (49-0) of the space shuttle orbiter in the NASA/Ames 3.5-foot hypersonic wind tunnel (OA87)

Petrozzi, M. T.
Mellenthin, J. A.
Milam, M. D.

February 1974

Experimental aerodynamic investigations were conducted on a scale model of the space shuttle orbiter...

Results of investigations on a 0.015-scale model 2A configuration of the Rockwell International space shuttle orbiter in the NASA/Ames Research Center 3.5 foot hypersonic wind tunnel

Mellenthin, J. A.
Nichols, M. E.
Milam, M. D.

September 1973

Experimental aerodynamic investigations were conducted in the NASA/Ames 3.5-Foot Hypersonic wind Tun...

Wind tunnel test of the 0.010-scale space shuttle integrated vehicle in the NASA-Ames 3.5 foot hypersonic wind tunnel (IA10)

Fitzgerald, F. F.
Mellenthin, J. A.
Cleary, J. W.
Petrozzi, M. T.

December 1973

Experimental aerodynamic investigations were conducted in the NASA Ames Research Center 3.5-Foot Hyp...

Results of transonic tests in the NASA/MSFC 14-inch trisonic wind tunnel on a 0.004-scale model (74-OTS) space shuttle launch vehicle (FA25)

Lundy, T. E.

January 1979

The primary objective of the test was to determine the aerodynamic increments due to the attach stru...

Results of investigations on an 0.015-scale configuration 140A/B space shuttle vehicle orbiter model (49-0) in the NASA/Langley Research Center 8-foot transonic pressure tunnel (OA25)

Nichols, M. E.

February 1974

Aerodynamic force and moment tests were conducted on an 0.015-scale space shuttle vehicle configurat...

Supersonic control effectiveness for full and partial span elevon configurations on a 0.0165 scale model space shuttle orbiter tested in the LaRC unitary plan wind tunnel (LA49)

March 1977

A wind tunnel test is reported on an early version of the space shuttle orbiter (designated 089B-139...

Results of transonic wind tunnel tests on an 0.010-scale space shuttle mated vehicle model 72-OTS in the LaRC 8-foot TPT (IA43)

Milam, M. D.
Petrozzi, M. T.

April 1975

Experimental aerodynamic investigations were conducted in NASA/Langley 8-Foot transonic pressure tun...

Investigations on an 0.030-scale space shuttle vehicle configuration 140A/B orbiter model in the Ames Research Center unitary plan 8 by 7-foot supersonic wind tunnel (0A53C)

Nichols, M. E.

July 1974

A wind tunnel test was conducted of an 0.030 scale model of the space shuttle orbiter in a supersoni...

Subsonic and transonic aerodynamic characteristics associated with variations in the geometry of the forward portion of irregular planform wings on a .01875 scale LO-100 Langley concept space shuttle orbiter in the Langley 8 foot TPT (LA7B)

Vaughn, J. E.
Poucher, D. E.

March 1973

The experimental longitudinal-and lateral-directional stability characteristics of a Langley concept...

Wind tunnel tests of an 0.015-scale configuration 140A/B space shuttle orbiter model (67-0) in the NASA/LRC 8-foot TPT to obtain transonic aerodynamic force data (OA106)

Burrows, R. R.

October 1974

These tests were conducted to obtain longitudinal stability and control data for Mach numbers from 0...

Terminal area energy management regime investigations utilizing an 0.030-scale model (47-0) of the space shuttle vehicle orbiter configuration 140A/B/C/R in the Ames Research Center 11 x 11 foot transonic wind tunnel (OH/48)

Hawthorne, P. J.

July 1976

Data obtained in a wind tunnel test were examined to: (1) obtain pressure distributions, forces and ...

Wind tunnel tests of the 0.010-scale space shuttle integrated vehicle (model 52-QT) in the NASA/Ames 3.5-foot hypersonic wind tunnel (IA18)

Stone, J.
Chee, E.
Mellenthin, J. A.
Esparza, V.

March 1975

Experimental aerodynamic investigations were conducted in the NASA/Ames Research Center 3.5-foot hyp...

Results of investigations on an 0.015 scale 140A/B configuration space shuttle vehicle orbiter model (49-0) in the LTV 4 by 4-foot high speed wind tunnel (0A84)

Esparza, V.
Embury, W. R.

August 1974

Data obtained from a wind tunnel test of an 0.015-scale 140 A/B configuration space shuttle vehicle ...

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...

Subsonic, transonic, and supersonic stability and control characteristics of the -147B space shuttle orbiter

Mennell, R. C.

October 1973

Experimental aerodynamic investigations were conducted on 0.015 scale representations of two Space S...

Results of investigations on a 0.015-scale model (49-0) of the space shuttle orbiter in the NASA/Ames 3.5-foot hypersonic wind tunnel (OA87)

Petrozzi, M. T.
Mellenthin, J. A.
Milam, M. D.

February 1974

Experimental aerodynamic investigations were conducted on a scale model of the space shuttle orbiter...

Results of investigations on a 0.015-scale model 2A configuration of the Rockwell International space shuttle orbiter in the NASA/Ames Research Center 3.5 foot hypersonic wind tunnel

Mellenthin, J. A.
Nichols, M. E.
Milam, M. D.

September 1973

Experimental aerodynamic investigations were conducted in the NASA/Ames 3.5-Foot Hypersonic wind Tun...

Wind tunnel test of the 0.010-scale space shuttle integrated vehicle in the NASA-Ames 3.5 foot hypersonic wind tunnel (IA10)

Fitzgerald, F. F.
Mellenthin, J. A.
Cleary, J. W.
Petrozzi, M. T.

December 1973

Experimental aerodynamic investigations were conducted in the NASA Ames Research Center 3.5-Foot Hyp...

Results of transonic tests in the NASA/MSFC 14-inch trisonic wind tunnel on a 0.004-scale model (74-OTS) space shuttle launch vehicle (FA25)

Lundy, T. E.

January 1979

The primary objective of the test was to determine the aerodynamic increments due to the attach stru...

Results of investigations on an 0.015-scale configuration 140A/B space shuttle vehicle orbiter model (49-0) in the NASA/Langley Research Center 8-foot transonic pressure tunnel (OA25)

Nichols, M. E.

February 1974

Aerodynamic force and moment tests were conducted on an 0.015-scale space shuttle vehicle configurat...

Transonic control effectiveness for full and partial span elevon configurations on a 0.0165 scale model space shuttle orbiter tested in the LaRC 8-foot transonic wind tunnel (LA48)

Abstract

Extracted data

Transonic control effectiveness for full and partial span elevon configurations on a 0.0165 scale model space shuttle orbiter tested in the LaRC 8-foot transonic wind tunnel (LA48)

Abstract

Extracted data

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