INSERTION OF FUSION BONDED THERMOPLASTIC TECHNOLOGY INTO FLIGHT TESTING

VFS-F58-00094

6/11/2002

Authors
Abstract
Content

Many challenges and obstacles were overcome in order to get final flight test approval for the fusion-bonded thermoplastic stabilizer. The part and material system were subjected to a battery of tests. The design and environmental requirements, and loads, are evolving concurrently as development of this stabilizer continues. There were also fabrication and assembly enhancements required to achieve quality. This groundwork or basis for the flight testing, including risk reduction tests, manufacturing improvements, design changes, and evolving criteria for the fusion-bonded stabilizer, will be outlined and detailed.

Meta TagsDetails
DOI
https://doi.org/10.4050/VFS-F58-00094
Citation
Crane, D., Hethcock, J., Jones, R., Messinger, S., et al., "INSERTION OF FUSION BONDED THERMOPLASTIC TECHNOLOGY INTO FLIGHT TESTING," Forum 58 - Montreal, Canada 2002, Montreal, Canada, June 11, 2002, https://doi.org/10.4050/VFS-F58-00094.
Additional Details
Publisher
Published
6/11/2002
Product Code
VFS-F58-00094
Content Type
Technical Paper
Language
English