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    PELLET LOADED ATTITUDE CONTROL ROCKET MOTOR
    5.
    发明公开
    PELLET LOADED ATTITUDE CONTROL ROCKET MOTOR 有权
    佩莱OPERATED保持控制火箭

    公开(公告)号：EP2245291A2

    公开(公告)日：2010-11-03

    申请号：EP09739301.1

    申请日：2009-02-05

    申请人： Raytheon Company

    发明人： CAVALLERI, Robert ,  OLDEN, Thomas

    IPC分类号： F02K9/08

    CPC分类号： F02K9/08 ,  F02K9/10 ,  F02K9/18 ,  F02K9/36 ,  Y10T29/49346

    摘要： There is disclosed a solid fuel rocket motor (500) which may include a case (510) and a nozzle (540) coupled to the case. A plurality of fuel pellets (525) may be disposed within the case. An igniter (550) may be disposed to ignite at least a portion of the fuel pellets. A pellet retainer (535) may be positioned within the case to retain the plurality of fuel pellets within the case. The pellet retainer may be perforated to allow exhaust gases to flow from the ignited fuel pellets to the nozzle while preventing unburned fuel pellets from being expelled through the nozzle.

    INTEGRAL THRUST VECTOR AND ROLL CONTROL SYSTEM
    6.
    发明公开
    INTEGRAL THRUST VECTOR AND ROLL CONTROL SYSTEM 有权
    积分推力矢量和侧倾控制系统

    公开(公告)号：EP2297544A2

    公开(公告)日：2011-03-23

    申请号：EP09764938.8

    申请日：2009-05-19

    申请人： Raytheon Company

    发明人： KINSEY, Lloyd ,  CAVALLERI, Robert

    IPC分类号： F42B10/66

    CPC分类号： F42B10/665 ,  F02K9/90 ,  F02K9/978 ,  F05D2240/40 ,  F05D2250/411 ,  F05D2250/42

    摘要： An apparatus for vectoring the thrust of a motor that produces thrust along a longitudinal axis by expelling combustion gases through a nozzle (310) may include a plurality of linearly-positionable non-rotatable thrust deflectors (322, 325, 326, 328). The thrust deflectors (322, 325, 326, 328) may be disposed at around a perimeter of the nozzle (310). Each thrust deflector (322, 325, 326, 328) may be independently extended to simultaneously generate both a force (Fl, F2, F3, F4) transverse to the longitudinal axis (305) and a torque (Tl, T2, T3, T4 ) about the longitudinal axis (305).

    ROCKET MOTOR WITH PELLET AND BULK SOLID PROPELLANTS
    7.
    发明公开
    ROCKET MOTOR WITH PELLET AND BULK SOLID PROPELLANTS 有权
    佩莱和大量的固体燃料火箭发动机

    公开(公告)号：EP2281114A2

    公开(公告)日：2011-02-09

    申请号：EP09739312.8

    申请日：2009-02-10

    申请人： Raytheon Company

    发明人： CAVALLERI, Robert ,  OLDEN, Thomas

    IPC分类号： F02K9/10 ,  F02K9/12 ,  F02K9/18

    CPC分类号： F02K9/08 ,  F02K9/10 ,  F02K9/24 ,  F02K9/346

    摘要： There is disclosed a solid fuel rocket motor (500) which may include a case (510) and a nozzle (540) coupled to the case (510). A plurality of fuel pellets (525) may be disposed within the case (510). An igniter (550) may be disposed to ignite at least a portion of the fuel pellets (525). A pellet retainer (535) may be positioned within the case (510) to retain the plurality of fuel pellets (525) within the case (510). The pellet retainer (535) may be perforated to allow exhaust gases to flow from the ignited fuel pellets to the nozzle (540) while preventing unburned fuel pellets from being expelled through the nozzle (540).