3233. Fuel Analysis: Methods, Techniques, and Calibration

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Title3233. Fuel Analysis: Methods, Techniques, and Calibration
Publication TypeConference Paper
Paper Number3233
Year of Publication2002
AuthorsDaguia, Marie
Paper Category11.0. WEIGHT ENGINEERING - AIRCRAFT ESTIMATION
Conference61st Annual Conference, Virginia Beach, Virginia, May 18-22
Conference LocationVirginia Beach, Virginia
PublisherSociety of Allied Weight Engineers, Inc.
Date Published5/18/02
Abstract

This paper describes a specific method that can be used for fuel volume analysis and its associated mass properties. The fuel system for the X?47A Pegasus unmanned air vehicle an experimental aircraft designed and built by Northrop Grumman Integrated Systems, is used as a specific example to demonstrate this approach early in the design phase. Fuel tank volume is derived from solid models then adjusted for design allowances that correct for ullage and ISS (Internal Structure and Subsystems) components to derive realistic usable volume. Fuel table generation and center of gravity travel plots, including pitch attitude variation, are also discussed. Fuel calibration test data and comparison to analysis are presented.

Pages18
Key Words11. Weight Engineering - Aircraft Estimation
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