Technique for Verifying Structural Integrity of Full-Scale Segments of Launch Vehicles at Transonic Speeds
1967
17 pages
Report
No indication
English
Space Launch Vehicles & Support Equipment , Axisymmetric flow , Component reliability , Flight stability test , Launch vehicle , Transonic wind tunnel , Ac , Aeroelasticity , Aircraft , Axisymmetry , Centaur launch vehicle , Component , Cone , Flight , Flow , Free , Launch , Method , Model , Nose , Reliability , Segment , Stability , Test , Transonic , Tunnel , Validity , Vehicle , Wind