| 摘要 |
A hybrid rocket motor having a multitude of radially inward directed miniature hybrid secondary combustion chambers within a single solid fuel block being oxidizer-fed by a single centrally positioned distributor and a system of radially outward-directed feed tubes. The feed tubes are sealed at their distant ends and have multiple orifices opening into the secondary combustion chambers to resemble a multitude of secondary conventional-injection hybrid motors within a single main hybrid motor.
|
