Aeroelastic characteristics of the Space Shuttle external tank cabletrays
Author:
Affiliation:
1. Lockheed Missiles & Space Company, Sunnyvale, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25746
Reference23 articles.
1. Analysis of Static and Dynamic Wind Tunnel Tests of the Shuttle Cable Trays
2. Aeroelastic Stability of Space Shuttle Protuberances
3. Dynamic wind tunnel tests of the simulated Shuttle external cable trays
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