FUEL TANK PRESSURIZATION 'B' CONFIGURATION,

Abstract

The object of this test was to operationally check the airborne fuel tank pressurization system under the simulated booster condition, that exists just prior to and at booster separation. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 24, 1958
Accession Number
AD0830225

Entities

People

  • D. W. Kuhlman

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Airborne
  • Containers
  • Fuel Tanks
  • Pressurization

Readers

  • Aerospace Test and Evaluation
  • Petroleum Engineering