Antimisting Fuel (AMK) Flight Degrader Development and Aircraft Fuel System Investigation
-
1987-02-01
Details
-
Creators:
-
Corporate Creators:
-
Corporate Contributors:
-
Subject/TRT Terms:
-
Publication/ Report Number:
-
Resource Type:
-
Geographical Coverage:
-
Edition:Contract Final Report
-
Corporate Publisher:
-
Abstract:This report summarizes results from a 20-month technical effort involving the design, fabrication and evaluation of an Antimisting Kerosene (AMK) degrader. The principal objective was to demonstrate the feasibility of employing a high-speed centrifugal pump to condition AMK fuel for use in an aircraft turbine engine. The effects of AMK fuel on the engine/airframe fuel system as well as any effect the flight environment might have had on the fire-preventive characteristics of the AMK were also investigated.
-
Format:
-
Funding:
-
Collection(s):
-
Main Document Checksum:urn:sha-512:8baf83b440136c333f518a47375c2d4ef9f1a077322ffde4211f260b51aec68ed9ff552f41e2abb2700b259a40ad0ff35dd59671c3bf6738d4d0624aca58fd69
-
Download URL:
-
File Type: