Scale model studies of the Shuttle Orbiter arrestment system were conducted to determine the proper net arrestment system configuration to bring the Orbiter to a safe stop in the event of a runway overshoot. Areas of interest include the effect of various net geometries on net engagement of the nose gear and main gear; and whether or not the top bundle contacts the crew cabin window. The model tests indicated that the net arrestment system was properly designed to bring the Orbiter to a safe stop with minimal amount of damage. The test procedures and data are presented.
Shuttle Orbiter arrestment system studies
01.10.1988
Aufsatz (Konferenz)
Keine Angabe
Englisch
Shuttle Orbiter Arrestment System Studies
SAE Technical Papers | 1988
|Studies of Shuttle Orbiter Arrestment System
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NTRS | 1993
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