ROCKETONE AEROSPACE PTY LTD.
|ROCKETONE AEROSPACE PTY LTD. Patent applications|
|Patent application number||Title||Published|
|20090139204||Hybrid Rocket System - The present invention describes a hybrid rocket motor that includes a first solid reactant and at least one thrust nozzle and at least one moveable combustion control member within the hybrid rocket motor that restricts the contact of a first fluid reactant in the combustion chamber. In this way, it is then possible to regulate the exposure of the solid reactant to the fluid reactant and thus control thrust.||06-04-2009|