Destratification of Cryogenic Propellants,

Abstract

This document discusses destratification of cryogenic propellants. Various destratification systems are evaluated and compared. The axial and radial jet concepts are found to offer the best performance, simplicity, compactness and low system weight. The procedure for designing an axial or radial jet destratification system is shown in a sample problem. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1969
Accession Number
AD0865270

Entities

People

  • James B. Urquhart Iii

Organizations

  • Boeing

Tags

DTIC Thesaurus Topics

  • Cryogenic Propellants
  • Energetic Materials
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Propellants

Fields of Study

  • Physics

Readers

  • Environmental Engineering
  • Rocket Propulsion.
  • Software Engineering