Studies of Shuttle Orbiter Arrestment System

By: Nasa, National Aeronautics and Space Adm

Scale model studies of the Shuttle Orbiter Arrestment System (AS) were completed with a 1/27.5-scale model at the NASA Langley Research Center. The purpose of these studies was to determine the proper configuration for a net arrestment system to bring the orbiter to a safe stop with minimal damage in the event of a runway overrun. Tests were conducted for runway on-centerline and off-centerline engagements at simulated speeds up to approximately 100 knots (full scale). The results of these tests defined the interaction of the net and the orbiter, the dynamics of off-centerline engagements, and the maximum number of vertical net straps that may become entangled with the nose gear. In addition to these tests, a test program with a 1/8-scale model was conducted by the arrestment system contractor, and the results are presented in the appendix. Davis, Pamela A. and Stubbs, Sandy M. Langley Research Center...

• Format: Paperback
• Language: English
• ISBN: 1730989950
• ISBN13: 9781730989957
• Release Date: January 1
• Publisher: Independently Published
• Length: 96 Pages
• Weight: 0.54 lbs.
• Dimensions: 0.2" x 8.5" x 11.0"