Characteristics of ballistic missile and design of nose cone primary purpose of which is to provide thermal protection for payload; factors considered in study of Missile and Space Vehicle Dept of General Electric Co selecting material to protect Atlas re-entry nose cone at ICBM ranges; flight test program and method of obtaining data with copper heat sink re-entry vehicle over range of re-entry conditions.
Nose cones -- Case for heat sink
Missiles Rockets
Missiles and Rockets ; n 24
1959
3 pages
Article (Journal)
English
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