Study of Thermal Protection Requirements for a Lifting Body Entry Vehicle Suitable for Near-Earth Missions Final Report
1966
198 pages
Report
No indication
English
Physics , Manned Spacecraft , Abort trajectory , Lifting body , Reentry trajectory , Thermal protection , Ablation , Abort , Analysis , Body , Earth , Entry , Error , Field , Flow , Lifting , M- 2 lifting body , Mission , Near , Protection , Reentry , Saturn ib launch vehicle , Thermal , Titan ii icbm , Titan iii icbm , Trajectory , Vehicle