Atmospheric density, winds and turbulence relative influence on Saturn V vehicle control system and structural bending moment response during Atlantic Missile Range ascent flight
Relative influence of atmospheric properties on launch vehicle design.
1967-02-01
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Englisch
LAUNCH VEHICLE ATMOSPHERIC FLIGHT LOADS - Launch Vehicle Atmospheric Flight Loads
Online Contents | 2000
|Launch Vehicle Atmospheric Flight Loads
AIAA | 2000
|