RESULTS AND ANALYSIS OF THE HARDENED XNS17 GUIDANCE SECTION/FIG. A 1214.6A LIQUID COOLER EQUIPMENT COMPATIBILITY TEST,
BOEING CO SEATTLE WA
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This test report is in partial fulfillment of the requirements of a contract to design and develop a liquid cooler for the Wing VI NS 17 guidance section. The test which was conducted on prototype hardware was set up to simulate closely the silo configuration and environment. Photographs have been provided in the body of the report to show the equipment arrangement and the instrumentation used.
- Air Conditioning, Heating, Lighting and Ventilating
- Surface-Launched Guided Missiles