Static Longitudinal Aerodynamic Characteristics Of A Model Of A Two Stage Version Of A Saturn Launch Vehicle With A Proposed Apollo Payload At Mach Numbers From 157 To 287 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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