The present invention relates to throttleable propulsion launch escape systems and devices. In one embodiment, the system includes a tower and at least one throttleable motor secured to the tower. The throttleable motor is able to throttle to a reduced power setting during flight. In another embodiment, the system includes at least one throttleable motor and a space vehicle unit that includes a containing structure. In a further embodiment, the throttleable motor may be secured about a boost escape system of a space vehicle unit. In an additional embodiment, the present invention is a three-dimensional nozzle.
Throttleable Propulsion Launch Escape Systems and Devices
2018-02-01
Patent
Electronic Resource
English
Throttleable propulsion launch escape systems and devices
European Patent Office | 2020
|Throttleable Thrustor System Final Report
NTIS | 1970
|Throttleable thruster system Final report
NTRS | 1971
|