Accession Number : AD0865270

Title :   Destratification of Cryogenic Propellants,

Corporate Author : BOEING CO HUNTSVILLE AL LAUNCH SYSTEMS BRANCH

Personal Author(s) : Urquhart, James B., III

Report Date : 01 DEC 1969

Pagination or Media Count : 67

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)

Descriptors :   *HEAT TRANSFER), (*CRYOGENIC PROPELLANTS, (*PROPELLANT TANKS, HEAT TRANSFER), BLOWERS, LIQUID JETS, VENTING, HEAT EXCHANGERS, WEIGHT, DUCT INLETS, ROTATION, MIXTURES, DIELECTRICS, ELECTRODES, ELECTROPHORESIS, LIQUEFIED GASES, HYDROGEN, REYNOLDS NUMBER, THRUST, BOUNDARY LAYER, PUMPS, PENETRATION, BUBBLES, KINETIC ENERGY, SYSTEMS ENGINEERING, PROPELLANT CONTROL, SHROUDED PROPELLERS.

Subject Categories : Containers and Packaging
      Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE