Yaw Stabilization for Aircraft Ejection Seats.
Abstract
An aircraft ejection seat is provided with deployable fins for stabilizing yaw rotation. The fins are normally stowed along the sides of the ejection seat. During ejection, the fins are deployed aft of the seat by means of rotational actuators. Anti-entanglement sheets are collapsibly disposed between the fins and the sides of the seat in order to prevent fouling of the parachute. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 31, 1983
- Accession Number
- ADD010472
Entities
People
- Peter Ayoub
- Thomas Zenobi
Organizations
- United States Department of the Navy