Accession Number:

AD0269584

Title:

MAIN PROPELLANT TANK PRESSURIZATION SYSTEM STUDY AND TEST PROGRAM. VOLUME 3. DESIGN HANDBOOK

Descriptive Note:

Final rept.

Corporate Author:

LOCKHEED AIRCRAFT CORP MARIETTA GA

Personal Author(s):

Report Date:

1961-12-01

Pagination or Media Count:

111.0

Abstract:

Design information on liquid propellant tank pressurization systems is presented. The areas covered are pressurization gas requirements, including hand calculation procedures and nomographs tankage, including material properties and volume and wall area curves and components, including stored He system weight curves and a simple but accurate heat exchanger design method.

Subject Categories:

  • Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE