Accession Number : AD0842153

Title :   GEYSERING STUDY LOX TRANSFER SYSTEM (HIGH TOWER) MODEL 55 - CENTAUR,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Gere, I. N.

Report Date : 23 JUN 1960

Pagination or Media Count : 13

Abstract : This report is aimed at studying the causes and effects of geysering into the missile tank, and investigating the minimum flow required to prevent geysering and top off the missile. (Author)

Descriptors :   *CRYOPUMPING), (*LAUNCH VEHICLES, PROPELLANT TRANSFER), (*CRYOGENIC PROPELLANTS, LIQUEFIED GASES, OXYGEN, BOILING, FLUID FLOW, PROPELLANT TANKS, PRESSURIZATION, PUMPS, CAVITATION.

Subject Categories : Liquid Rocket Propellants
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE