METHOD OF EJECTION OF FLYING VEHICLE CREW MEMBER Russian patent published in 1995 - IPC

FIELD: space engineering. SUBSTANCE: force is applied to ejection seat 1 which is directed at eccentricity relative to center of masses of "ejection seat crew member" system and seat is brought out of flying vehicle 2 with head-rest forward. Then initial section 4 of trajectory path of seat 1 is formed by applying force to it at eccentricity till trajectory is inclined to horizon at angle of 45 to 50 deg, after which seat 1 is stabilized and direction of force action is changed orienting it through center of masses of "ejection seat-crew member" system in parallel with seat back. EFFECT: increased range of throwing the seat in ejecting it from space vehicle at launch and injection. 1 dwg