A high energy catapult assembly may comprise an outer tube and an inner tube located within the outer tube. The outer tube may be configured to telescope relative to the inner tube. A propellant cartridge may be located in an inner tube chamber of the inner tube. An actuator may be configured to change an open volume of the inner tube chamber.
VARIABLE VOLUME HIGH ENERGY CATAPULT ASSEMBLIES FOR EJECTION SYSTEMS
2022-10-20
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Variable volume high energy catapult assemblies for ejection systems
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