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3% Crew Exploration Vehicle (CEV) Command Module and Launch Abort Tower

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NASA

Nov 30, 2012
Image Article
model of Space Shuttle in a wind tunnel
Test to investigate aerodynamic proximity and jettison motor plume interaction effects on the separation of the crew module from the launch abort tower during an abort from the Ares launch vehicle.

Test to investigate aerodynamic proximity and jettison motor plume interaction effects on the separation of the crew module from the launch abort tower during an abort from the Ares launch vehicle.