Stress Analysis Of The External Front Window Of The X-20a (Dyna-Soar)

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Report Number: SEG TDR 64-16
Author(s): Johnson, Verner J.
Corporate Author(s): Systems Engineering Group Research And Technology Div Wright-Patterson AFB Ohio
Date of Publication: 1964-06
Pages: 44
DoD Task:
Identifier: AD0603356

This report was prepared by personnel of the X-20 Engineering Office. It is the stress analysis of the external front window of the X-20A. The author especially acknowledges the help of task engineers Laslow Berke and James Johnson of the Air Force Flight Dynamics Laboratory in the use of the computer program and for their aid in this study. X -20 Engineering Office Project Engineers, W. D. Cowie and Captain R. J. Meyette, supplied drawings of the window and the design pressure distribution for that window, respectively. Messrs. R. M. Bader and F. Campanile derived the temperature distribution.

Provenance: Lockheed Martin Missiles & Fire Control

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