Abstract
The intricate pattern of stresses and strains induced in missile structures by the combined environments encountered during re-entry of the earth's atmosphere has necessitated the establishment of unique testing techniques and facilities for evaluating missile performance during this severe phase of flight.
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Bibliography
Howell, A. J., Simulating Re-Entry Flight of Ballistic Missiles, Chrysler Corp. Missile Division, 4/15/59, CO62 Pub. 50 (unclassified).
Smith, George A., Stress Rupture Data for A151, 304, 321 and Armco 17-7 PH Stainless Steels, Chrysler Missile Division, Technical Memorandum MT-M34, April 1957 (unclassified).
Smith, M. C., External Heating of Ballistic Missiles, Chrysler Corp-Missile Division, Technical Report AD-R3, July 21, 1955 (unclassified).
Additional information
R. T. Nichols was formerly associated with Chrysler Corp., Detroit, Mich.; is now employed by Lockheed Missiles and Space Div., Sunnyvale, Calif.
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Nichols, R.T. Testing techniques for full-scale missile structures under simulated re-entry environment. Experimental Mechanics 1, 8–15 (1961). https://doi.org/10.1007/BF02324902
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DOI: https://doi.org/10.1007/BF02324902