3 ms·
Because of the engine failures, thrust wasn't as high as it would be in a nominal flight, so max aerodynamic pressure was lower. It didn't hit the max Q it woul
by sbierwagen 4y ago
Because of the engine failures, thrust wasn't as high as it would be in a nominal flight, so max aerodynamic pressure was lower. It didn't hit the max Q it would experience in a regular launch.