|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02K-009/08 B64G-001/26 F42B-010/66 B64G-001/40|
|우선권정보||FR-11 01524 (2011-05-19)|
|§371/§102 date||20131227 (20131227)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 5|
A system for in-flight attitude control and side-force steering includes a thruster body and a plurality of valves capable of generating side thrusts put into communication with the thruster body. The valves are arranged in two sets of valves spaced apart from each other towards the front and towards the rear of the thruster body in substantially symmetrical manner relative to the center of gravity of the vehicle situated on a longitudinal axis (A) of the vehicle. Each set comprises a first pair of valves generating thrust in opposite directions along ax...
1. A system for providing a vehicle with in-flight attitude control and side force steering, the system comprising: a thruster body and a plurality of valves capable of generating side thrusts by being put into communication with the thruster body by means of a control device arranged to act individually on each valve;wherein the valves are distributed in first and second sets of valves, the two sets being disposed at a distance apart from each other respectively towards the front and towards the rear of the thruster body in a manner that is substantiall...