Accession Number : AD0856893
Title : Gemini B Oxygen System Venturi and Umbilical Evaluation of Flow Characteristics.
Descriptive Note : Final rept.
Corporate Author : MCDONNELL AIRCRAFT CO ST LOUIS MO
Report Date : 14 FEB 1969
Pagination or Media Count : 27
Abstract : A venturi was developed to prevent flow sharing of the secondary oxygen system with the primary oxygen system during cabin repressurization. The resultant venturi is utilized in the oxygen system during crewman transfer with the crew transfer umbilical. This test measured the flow characteristics of the series connected combination of the venturi, the cabin repressurization valve and the CTUM (25 foot and 43 foot configurations) with various specified pressures at the inlet to the venturi. (Author)
Descriptors : (*MANNED SPACECRAFT, OXYGEN EQUIPMENT), (*SPACE STATIONS, OXYGEN EQUIPMENT), (*OXYGEN EQUIPMENT, GAS FLOW), SPACE CAPSULES, OXYGEN, PRESSURIZED CABINS, UMBILICAL CORDS(AEROSPACE), VENTURI TUBES.
Subject Categories : Manned Spacecraft
Life Support Systems
Distribution Statement : APPROVED FOR PUBLIC RELEASE