This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Fuel Transfer System in the Conceptual Design Phase
Technical Paper
2002-01-2931
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Language:
English
Abstract
As the time between different development projects of new aircraft (a/c) extends, experienced personnel in the field of basic a/c system design are difficult to employ when being on the onset of a new design. Further on basic a/c system design is a field neglected in literature and in the educational system.
A text is under development that summarizes the Saab experience of the complete fuel system design with respect to the fighter a/c Viggen and Gripen, the commuter a/c 340 and 2000, the trainer a/c SK60 and also the conceptual a/c B3LA.
This paper is an extract of this text and describe early considerations that have to be made when designing a fuel transfer system. Emphasis is put on the top requirements on a/c level.
Recommended Content
Authors
Citation
Gavel, H., "Fuel Transfer System in the Conceptual Design Phase," SAE Technical Paper 2002-01-2931, 2002, https://doi.org/10.4271/2002-01-2931.Also In
References
- JSSG JSSG 2009 Appendix E 1998 Joint Service Specification Guide
- Navair Navair 06-5-504 1967 Fuel and Fuel Systems