Accession Number : AD0477549
Title : INVESTIGATION OF FIRE EXTINGUISHING SYSTEM REQUIREMENTS FOR ADVANCED FLIGHT VEHICLES.
Descriptive Note : Final rept. Jan 65-Jan 66,
Corporate Author : NATIONAL ENGINEERING SCIENCE CO PASADENA CA
Personal Author(s) : Landesman, Herbert ; Klusmann, Eugene B. ; Minich, John ; Christiansen, Gorm
Report Date : JAN 1966
Pagination or Media Count : 324
Abstract : Data are presented defining thermal stability limits for model structures of fluorinated chloro- and bromo-carbons suitable for use as fire extinguishing agents. Heating analyses have been made for an idealized extinguishant tank subjected to various flight regimes. Insulation thicknesses as well as example calculations of weight penalties due to insulation necessary to maintain temperatures below decomposition have been computed for various extinguishants in the idealized tank under Mach 4 and 5 regimes. A literature survey and study of the feasibility of using dry powder extinguishants as in-flight extinguishants has been made. Problems which may be encountered are discussed. (Author)
Descriptors : *FIRE EXTINGUISHERS), (*SUPERSONIC AIRCRAFT, FEASIBILITY STUDIES, HALOGENATED HYDROCARBONS, THERMAL INSULATION, THERMAL PROPERTIES, FIRE RESISTANT COATINGS, AIRCRAFT FIRES, STABILITY, AERODYNAMIC HEATING, SURFACE TEMPERATURE, AIRFRAMES, SUPERSONIC FLIGHT, SYNTHESIS(CHEMISTRY), HEAT TRANSFER, SKIN FRICTION, HEAT EXCHANGERS, TEMPERATURE, BROMINE COMPOUNDS, CHLORINE COMPOUNDS, FLUORINE COMPOUNDS, POWDERS, ALKALI METAL COMPOUNDS, HALIDES, CHEMICAL PROPERTIES, DECOMPOSITION.
Subject Categories : Aircraft
Ceramics, Refractories and Glass
Distribution Statement : APPROVED FOR PUBLIC RELEASE