Accession Number:

AD0829132

Title:

RESULTS AND ANALYSIS OF THE HARDENED XNS17 GUIDANCE SECTION/FIG. A 1214.6A LIQUID COOLER EQUIPMENT COMPATIBILITY TEST,

Descriptive Note:

Corporate Author:

BOEING CO SEATTLE WA

Personal Author(s):

Report Date:

1965-04-07

Pagination or Media Count:

449.0

Abstract:

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.

Subject Categories:

  • Air Conditioning, Heating, Lighting and Ventilating
  • Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE