The three-man Rotor Systems Research Aircraft (RSRA) Emergency Escape System, the first system known to be fully qualified and operational in a rotary wing aircraft, will have two modes of operation: one providing for full in-flight egress, and the other for the severance of the rotor blades for a return to base as a fixed-wing aircraft. This paper describes the escape system's design principles, integration into the aircraft, qualification, and performance.
Helicopter emergency escape
Survival and Flight Equipment Association, Annual Symposium ; 1978 ; San Diego, CA
1979-01-01
Sonstige
Keine Angabe
Englisch
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