Wind Tunnel Investigation Of The Static Longitudinal Aerodynamic Characteristics Of Several Configurations Of A Proposed Little Joe 2 Apollo Space Vehicle At Mach Numbers From 030 To 120 PDF Download

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Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II-Apollo Test Vehicle at Mach Numbers from 0.056 to 4.65

Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II-Apollo Test Vehicle at Mach Numbers from 0.056 to 4.65
Author: Robert H. Moore
Publisher:
Total Pages: 236
Release: 1968
Genre: Launch vehicles (Astronautics)
ISBN:

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Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Models of Reentry and Atmospheric-abort Configurations of a Proposed Apollo Spacecraft at Mach Numbers from 0.30 to 1.20

Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Models of Reentry and Atmospheric-abort Configurations of a Proposed Apollo Spacecraft at Mach Numbers from 0.30 to 1.20
Author:
Publisher:
Total Pages: 28
Release: 1961
Genre:
ISBN:

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Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of a Modified Model of a Proposed Apollo Atmospheric Abort Configuration at Mach Numbers from 0.30 to 1.20

Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of a Modified Model of a Proposed Apollo Atmospheric Abort Configuration at Mach Numbers from 0.30 to 1.20
Author: Albin O. Pearson
Publisher:
Total Pages: 22
Release: 1962
Genre:
ISBN:

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NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 562
Release: 1967
Genre:
ISBN:

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Total Pages: 478
Release: 1968
Genre: Aeronautics
ISBN:

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