In the tractor-rocket seated-extraction candidate system for Space Shuttle Orbiter crew escape, the crewmember is pulled from his seat and away from the Orbiter via an elastic pendant, using a system of rails to guide the extraction trajectory through an opening on the window frame for flight deck crew and through the side hatch for the middeck crew. A three-body simulation has been developed to model the flight-mechanics aspects of the concept, where the three bodies are the astronaut (six DOF), the tractor rocket (six DOF), and the Shuttle Orbiter (three DOF); attention is given to crewmembers' clearance of the Orbiter structure and engine plumes.
A three body dynamic simulation of a seated tractor rocket escape system for the Space Shuttle
AIAA Atmospheric Flight Mechanics Conference ; 1989 ; Boston, MA, United States
1989-01-01
Conference paper
No indication
English
Dynamic Response of Human Body Seated on a Tractor and Effectiveness of Suspension Systems
Automotive engineering | 1977
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