Contents: Launch System Considerations--The Economic Feasibility of the Rocket Approach to Reusable Launch Systems, Application of Emergency Detection and Decision Systems to Launch Vehicles; Reentry and Recovery--Maneuver Characteristics of a Tactical Re-entry Vehicle with an Offset Center of Gravity, Determination of Re-entry Performance of the M-2 Lifting Body Based on Aerodynamic Heating Considerations, Considerations in the Design of Vehicles Capable of Substantial Hypersonic Lift-Drag Ratios, Hypersonic Dynamic Stability of Sharp and Blunt Slender Cones, The ASSET Recovery System, The Apollo Earth Landing System; Materials--Heat Protection by Radiative Heat Rejection, Polymers in Missiles and Space, Expandable Structures for Space Applications; Blast Simulation-- Explosive Simulation of Nuclear Blast on Test Vehicles, A Technique for Simulating Air-Blast-Induced Ground Motions, and others.
Transactions of the Symposium on Ballistic Missile and Space Technology (9th) Held at the United States Naval Training Center, San Diego, California on 12-14 August 1964. Volume II. Launch System Considerations, Re-Entry and Recovery, Materials, Blast Simulation, InspecTion, Space Station Logistics
1964
520 pages
Report
Keine Angabe
Englisch
Astronautics , Military Intelligence , Manned Spacecraft , Spacecraft Trajectories & Flight Mechanics , Space Launch Vehicles & Support Equipment , Symposia , Guided missiles , Spacecraft , Recoverable booster motors , Launch vehicles(Aerospace) , Malfunctions , Detection , Command + control systems , Reentry vehicles , Maneuverability , Tactical weapons , Boost-glide vehicles , Aerodynamic heating , Aerodynamic configurations , Design , Hypersonic characteristics , Recovery , Conical bodies , Parachutes , Heat shields , Polymers , Expanded plastics , Extendable structures , Nuclear explosions , Simulation , Blast , Space surveillance systems , Aerial cameras , Space stations , Logistics
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