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    • 3. 发明专利
    • THRUSTER DEVICE
    • JP2002317700A
    • 2002-10-31
    • JP2001125947
    • 2001-04-24
    • NAT SPACE DEV AGENCYMITSUBISHI HEAVY IND LTD
    • KOBAYASHI YOSHITAKAMIKI YOICHIRO
    • B64G1/26F02K9/60
    • PROBLEM TO BE SOLVED: To provide a thruster device capable of suppressing cost increase by suppressing the number of part items and establishing a stable combustion at all times. SOLUTION: The thruster device 1 includes a body 2, thrust force changing member 3, nozzle 4, fuel supplying means 5, and an oxidator supplying means 6. The device body 2 constitutes the contour of the device 1, while the thrust force changing member 3 is supported rotatably inside the device body 2, and the nozzle 4 is connected with the device body 2. The fuel supplying means 5 is furnished with a fuel manifold 21 and a fuel injection nozzle 22 which opens at the manifold 21 and inside the nozzle 4, while the oxidator supplying means 6 is furnished with an oxidator manifold 31 and an oxidator injection nozzle 32 which is open at the manifold 31 and inside the nozzle 4. The fuel injection nozzle 22 and oxidator injection nozzle 32 are furnished with major diametric nozzles 25 and 35 having a comparatively large flow section area and minor diametric nozzles 26 and 36 having a relatively small flow section area, respectively.