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

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.

Document Details

Document Type
Technical Report
Publication Date
Apr 07, 1965
Accession Number
AD0829132

Entities

People

  • J. A. Lee

Organizations

  • Boeing

Tags

DTIC Thesaurus Topics

  • Contracts
  • Environment
  • Guidance
  • Instrumentation
  • Photographic Materials
  • Photographs
  • Photography
  • Prototypes

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Software Engineering
  • Thermal Physics or Thermal Science.