Accession Number:

AD0829628

Title:

PROPELLANT UTILIZATION SYSTEM XSM-65B1 THRU B13 COMPONENTS TEST REQUIREMENTS,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1957-04-09

Pagination or Media Count:

22.0

Abstract:

The requirements listed herein contain the important or vital Parameters deemed necessary to insure proper operation of the Assemblies, Sub-Assemblies and Components of the Propellant Utilization System. Author

Subject Categories:

  • Surface-Launched Guided Missiles
  • Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE