Accession Number : AD0370481
Title : FUEL SYSTEM Z((XQ-5-1))ZFLOW RATE TESTS.
Corporate Author : LOCKHEED AIRCRAFT CORP VAN NUYS CALIF
Personal Author(s) : Abramoski,J. W.
Report Date : 02 AUG 1956
Pagination or Media Count : 35
Abstract : A series of tests was run to determine the fuel flow characteristics of the fuel system in horizontal, 30 degrees climb and dive attitudes. The total fuel flow supplied to the engine was found to be satisfactory at all attitudes tested, even though the individual tank flow contribution and time of exhaustion varied with attitude. (Author)
Descriptors : (*FUEL SYSTEMS, FLUID FLOW) (U) FUEL TANKS, CENTER OF GRAVITY, ACCELERATION, NITROGEN, TEMPERATURE, PRESSURE, EXPERIMENTAL DATA, DRONES, GASOLINE, INSTRUMENTATION
Subject Categories : Fuels
Distribution Statement : APPROVED FOR PUBLIC RELEASE