MAIN PROPELLANT TANK PRESSURIZATION SYSTEM STUDY AND TEST PROGRAM. VOLUME IV. COMPUTER PROGRAM

Abstract

A COMPUTER PROGRAM WHICH CAN BE USED TO DETERMINE THE PRESSURIZING GAS REPUIREMENTS FOR A MISSILE PROPELLANT TANK PRESSURIZATION SYSTEM IS DESCRIBED. The program is applicable to both cryogenic and storable propellants when pressurized with stored gas, evaporated propellant, and main tank injection methods of pressurization. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1961
Accession Number
AD0269553

Entities

Organizations

  • Lockheed Martin

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Computer Programs
  • Computers
  • Pressurization
  • Propellant Tanks
  • Propellants

Fields of Study

  • Physics

Readers

  • Computer Science.
  • Rocket Propulsion.