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Triton 2 (1B)The goal of this project was to perform a detailed design analysis on a conceptually designed preliminary flight trainer. The Triton 2 (1B) must meet the current regulations in FAR Part 23. The detailed design process included the tasks of sizing load carrying members, pulleys, bolts, rivets, and fuselage skin for the safety cage, empennage, and control systems. In addition to the regulations in FAR Part 23, the detail design had to meet established minimums for environmental operating conditions and material corrosion resistance.
Document ID
19950006223
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clark, Michelle L.
(Embry-Riddle Aeronautical Univ. Daytona Beach, FL, United States)
Meiss, A. G.
(Embry-Riddle Aeronautical Univ. Daytona Beach, FL, United States)
Neher, Jason R.
(Embry-Riddle Aeronautical Univ. Daytona Beach, FL, United States)
Rudolph, Richard H.
(Embry-Riddle Aeronautical Univ. Daytona Beach, FL, United States)
Date Acquired
September 6, 2013
Publication Date
May 3, 1994
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-197188
NAS 1.26:197188
Report Number: NASA-CR-197188
Report Number: NAS 1.26:197188
Accession Number
95N12636
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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