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ablation material absorbed aerodynamic Aerospace altitude astronaut attitude control Avco ballistic missile re-entry beryllium blunt body blunt shapes burnout velocity Cape Kennedy capsule Control Center cooling copper deceleration density devices earth satellites earth's atmosphere effect energy engines equipment feet per second ft/sec graphite gross launch weight ground stations guidance heat protection heat transfer heat-sink heating rate high temperatures hypersonic ICBM instruments ionized landing liquid magnetohydrodynamic Mars metal method of heat Missile and Space moon NACA NASA nautical miles necessary nose cone design obtain orbit oxygen payload phase planets pounds pressure probes radiation range re-entry body re-entry heating re-entry problems re-entry vehicle re-entry velocity rocket shock tube shock tunnel shown in Figure simulated space flight space missions Space Technology Laboratories space vehicle specific impulse stagnation point surface tantalum techniques telemetry thermal conductivity tion tracking trajectory typical U. S. Air Force wind tunnels