Ablative composite assemblies and joining methods thereof
Augmentor liner support band having finger positioners
Expandable nozzle mechanism for a rocket engine
Non-radiating extendible cloth exit cone for rocket nozzles
Nozzle assembly for a reaction engine
Propeller nozzles thereby reducing lateral forces
Reduced temperature sensitivity launch motor
Rocket engine nozzle with an engine diffuser
Stepped nozzle
Swing disc nozzle structure for ramjet engine
Thrust control nozzle for rockets
Two-position nozzle