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This technical note presents the aerodynamic damping measurements of a 0.02-scale model of the Saturn SA-1 launch vehicle vibrating in its first free-free bending mode, conducted at various Mach numbers and dynamic pressures. The study included configurations with rigid stabilizing fins and a winged spacecraft, finding that aerodynamic damping was small and stabilizing across all configurations tested. The results were compared with theoretical predictions, showing erratic agreement but good correlation wit

Author

thetomatron3000

Language

EN