Study of Thermal Protection Requirements for a Lifting Body Entry Vehicle Suitable for Near-Earth Missions Summary Report
1966
16 pages
Report
No indication
English
Physics , Manned Spacecraft , Lifting body , Reentry vehicle , Structural weight , Thermal protection , Ablation , Alloy , Elastomer , M- 2 lifting body , Material , Nylon , Phenol , Radiation , Refractory , Rene 41 , Shield