A fitting for use with an ejection seat system of an aircraft includes a fitting bar configured to extend across a top of a catapult of the ejection seat system and defining an angled slot configured to receive a portion of a gas port of the ejection seat system. The fitting further includes a first leg and a second leg coupled to and extending away from the fitting bar and configured to be pivotally coupled to a smokestack structure of the ejection seat system.
SPACE SAVER FITTING FOR EJECTION SEAT CATAPULT
31.03.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Development of RESCU (rocket ejection seat catapult, upward) mark 1
Engineering Index Backfile | 1957
|Optimal catapult impulse shaping for ejection seats
AIAA | 1984
|