Scale model studies of the Shuttle Orbiter Arrestment System have been completed. The system was tested with a 1/27.5 scale model at the NASA Langley Research Center and a 1/8 scale model at All American Engineering Company. The purpose of these studies was to determine the proper net arrestment system configuration to bring the Orbiter to a safe stop in the event of a runway overrun with minimal damage. Tests were conducted for centerline engagements and off-center engagements at simulated speeds up to 95 knots full scale. The results of these studies defined the net-orbiter interaction, corrections to prevent underwing engagements, corrections necessary to prevent net entanglement in the main gear, the dynamics of off-centerline engagements, and the maximum number of vertical straps that might become entangled with the nose gear.
Shuttle Orbiter Arrestment System Studies
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1988
01.10.1988
Aufsatz (Konferenz)
Englisch
Gears , Scale models , Runways
Shuttle Orbiter arrestment system studies
NTRS | 1988
|Studies of Shuttle Orbiter Arrestment System
NTIS | 1993
|Studies of Shuttle orbiter arrestment system
NTRS | 1993
|NTIS | 1980
|NTIS | 1979
|