Results of several experimental investigations of the static aerodynamic characteristics for the Apollo/Saturn 5 launch vehicle

Static longitudinal aerodynamic characteristics of several configurations used in the development of the Little Joe 2-Apollo test vehicle at Mach numbers from 0.056 to 4.65

Moore, R. H., Jr.

May 1968

Static longitudinal aerodynamic characteristics of configurations used in Little Joe/Apollo test veh...

Aerodynamic stability characteristics of the Apollo command module

Graham, R. E.
Moseley, W. C., Jr.
Hughes, J. E.

August 1968

Wind tunnel test data on static and dynamic stability of Apollo command module configuratio

Static aerodynamic characteristics of the aborted Apollo-Saturn IB vehicle

Nunley, B. W.

March 1966

Static aerodynamic characteristics of aborted Apollo-Saturn vehicles with normal force coefficient d...

Transonic aerodynamic characteristics of a saturn ib-apollo launch vehicle with various upper-stage configurations

Carter, C. R.

June 1965

Transonic wind pressure tunnel investigation for aerodynamic characteristics of Saturn IB APOLLO la...

A Supersonic/Hypersonic Aerodynamic Investigation of the Saturn 1B/Apollo Upper Stage

January 1966

The static stability and axial force characteristics of an upper stage Saturn 1B/Apollo model were i...

Correction of four-percent Saturn 5 model protuberance test data

Mc Canless, G. F., Jr.

April 1970

Data reduction of transonic wind tunnel static pressure variation tests for correcting Saturn 5 dat

Static stability and axial force characteristics of a 1.32 percent scale model of the Saturn IB/Apollo, its components, and the Saturn IB/Apollo/Minuteman launch vehicle, determined by wind tunnel test

Chianese, F.

September 1965

Wind tunnel stability tests of scale model Saturn IB/Apollo, and Saturn IB/Apollo/ Minuteman launch ...

Aerodynamic characteristics determined during development of the Apollo launch escape vehicle configuration

Bowen, F. E.
Moseley, W. C., Jr.

June 1969

Aerodynamic characteristics determined during development of Apollo launch escape vehicle configurat...

The aeroelastic characteristics of the Saturn-IB and Saturn-V launch vehicles

March 1965

Effects of flow separation on aeroelastic characteristics of Saturn IB and Saturn V launch vehicles ...

Transonic aerodynamic characteristics of a Saturn 1B Manned Orbiting Research Laboratory launch vehicle

Flechner, S. G.
Langhans, R. A.

August 1969

Wind tunnel investigation for determination of subsonic and transonic aerodynamic characteristics of...

Study of indicial aerodynamic forces of multistage space vehicle systems. Volume 1 - Application of theory to basic geometries and to the Saturn 5 Final report, 28 Jun. 1967 - 27 Sep. 1968

Blackburn, R. R.
Glauz, W. D.

September 1968

Potential theory for determining aerodynamic forces of axisymmetric vehicles and Saturn

Stability Characteristics of the Apollo Command Module

Moseley, W. C., Jr.
Hughes, J. E.
Moore, R. H., Jr.

March 1967

Wind tunnel tests of Apollo command module static and dynamic stability characteristic

Range safety data for Saturn SA-10

Solmon, G. W.
Leonard, E. L.

June 1965

Saturn SA-10 range safety data, and reliability analysis of S-IV-8 and S-IV-10 stage

AS-205/CSM-101 launch vehicle dynamics analyses, part 2

Colwell, C. L.

September 1968

Trajectory and dynamics analyses of Saturn 1B launch vehicle for Apollo-Saturn 205/CSM-101 missio

Some research related to the structural dynamics of launch vehicles

Runyan, H. L.

January 1965

Structural dynamics of Saturn I and Saturn V dynamic models - effect of ground wind on launch vehicl...

Static longitudinal aerodynamic characteristics of several configurations used in the development of the Little Joe 2-Apollo test vehicle at Mach numbers from 0.056 to 4.65

Moore, R. H., Jr.

May 1968

Static longitudinal aerodynamic characteristics of configurations used in Little Joe/Apollo test veh...

Aerodynamic stability characteristics of the Apollo command module

Graham, R. E.
Moseley, W. C., Jr.
Hughes, J. E.

August 1968

Wind tunnel test data on static and dynamic stability of Apollo command module configuratio

Static aerodynamic characteristics of the aborted Apollo-Saturn IB vehicle

Nunley, B. W.

March 1966

Static aerodynamic characteristics of aborted Apollo-Saturn vehicles with normal force coefficient d...

Transonic aerodynamic characteristics of a saturn ib-apollo launch vehicle with various upper-stage configurations

Carter, C. R.

June 1965

Transonic wind pressure tunnel investigation for aerodynamic characteristics of Saturn IB APOLLO la...

A Supersonic/Hypersonic Aerodynamic Investigation of the Saturn 1B/Apollo Upper Stage

January 1966

The static stability and axial force characteristics of an upper stage Saturn 1B/Apollo model were i...

Correction of four-percent Saturn 5 model protuberance test data

Mc Canless, G. F., Jr.

April 1970

Data reduction of transonic wind tunnel static pressure variation tests for correcting Saturn 5 dat

Static stability and axial force characteristics of a 1.32 percent scale model of the Saturn IB/Apollo, its components, and the Saturn IB/Apollo/Minuteman launch vehicle, determined by wind tunnel test

Chianese, F.

September 1965

Wind tunnel stability tests of scale model Saturn IB/Apollo, and Saturn IB/Apollo/ Minuteman launch ...

Aerodynamic characteristics determined during development of the Apollo launch escape vehicle configuration

Bowen, F. E.
Moseley, W. C., Jr.

June 1969

Aerodynamic characteristics determined during development of Apollo launch escape vehicle configurat...

The aeroelastic characteristics of the Saturn-IB and Saturn-V launch vehicles

March 1965

Effects of flow separation on aeroelastic characteristics of Saturn IB and Saturn V launch vehicles ...

Transonic aerodynamic characteristics of a Saturn 1B Manned Orbiting Research Laboratory launch vehicle

Flechner, S. G.
Langhans, R. A.

August 1969

Wind tunnel investigation for determination of subsonic and transonic aerodynamic characteristics of...

Study of indicial aerodynamic forces of multistage space vehicle systems. Volume 1 - Application of theory to basic geometries and to the Saturn 5 Final report, 28 Jun. 1967 - 27 Sep. 1968

Blackburn, R. R.
Glauz, W. D.

September 1968

Potential theory for determining aerodynamic forces of axisymmetric vehicles and Saturn

Stability Characteristics of the Apollo Command Module

Moseley, W. C., Jr.
Hughes, J. E.
Moore, R. H., Jr.

March 1967

Wind tunnel tests of Apollo command module static and dynamic stability characteristic

Range safety data for Saturn SA-10

Solmon, G. W.
Leonard, E. L.

June 1965

Saturn SA-10 range safety data, and reliability analysis of S-IV-8 and S-IV-10 stage

AS-205/CSM-101 launch vehicle dynamics analyses, part 2

Colwell, C. L.

September 1968

Trajectory and dynamics analyses of Saturn 1B launch vehicle for Apollo-Saturn 205/CSM-101 missio

Some research related to the structural dynamics of launch vehicles

Runyan, H. L.

January 1965

Structural dynamics of Saturn I and Saturn V dynamic models - effect of ground wind on launch vehicl...

Static longitudinal aerodynamic characteristics of several configurations used in the development of the Little Joe 2-Apollo test vehicle at Mach numbers from 0.056 to 4.65

Moore, R. H., Jr.

May 1968

Static longitudinal aerodynamic characteristics of configurations used in Little Joe/Apollo test veh...

Aerodynamic stability characteristics of the Apollo command module

Graham, R. E.
Moseley, W. C., Jr.
Hughes, J. E.

August 1968

Wind tunnel test data on static and dynamic stability of Apollo command module configuratio

Static aerodynamic characteristics of the aborted Apollo-Saturn IB vehicle

Nunley, B. W.

March 1966

Static aerodynamic characteristics of aborted Apollo-Saturn vehicles with normal force coefficient d...

Results of several experimental investigations of the static aerodynamic characteristics for the Apollo/Saturn 5 launch vehicle

Abstract

Extracted data

Results of several experimental investigations of the static aerodynamic characteristics for the Apollo/Saturn 5 launch vehicle

Abstract

Extracted data

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