公开(公告)号：WO2009151796A2

公开(公告)日：2009-12-17

申请号：PCT/US2009041240

申请日：2009-04-21

Applicant: RAYTHEON CO ,  OLDEN THOMAS A ,  CAVALLERI ROBERT J ,  KINSEY LLOYD E

Inventor： OLDEN THOMAS A ,  CAVALLERI ROBERT J ,  KINSEY LLOYD E

IPC: F42B10/64 ,  F42B10/66

CPC classification number: F42B10/64 ,  F42B10/668

Abstract: A solid-fuel pellet thrust and control actuation system (PT-CAS) provides command authority for maneuvering flight vehicles over subsonic and supersonic speeds and within the atmosphere and exo-atmosphere. The PT-CAS includes a chamber of solid-fuel pellets that are ignited to expel gas through a throat. The expelled gas is directed at supersonic vehicle speeds in atmosphere to a cavity between an aero control surface and the airframe to pressurize the cavity and deploy the surface or at subsonic speeds in atmosphere or any speed in exo-atmosphere allowed to flow out a through-hole in the surface where the throat and through-hole provide a virtual converging/diverging nozzle to produce a supersonic divert thrust. A pellet and control actuation system (P-CAS) without the through-hole provides command authority at supersonic speeds in atmosphere. A restrictor mechanism controls the bleed of pressurized gas from the cavity to the external environment to achieve a deployment time objective for either the PT-CAS or P-CAS.

Abstract translation: 固体燃料颗粒推力和控制致动系统（PT-CAS）为在亚音速和超音速下以及大气和大气中的机动飞行器提供了指挥权力。 PT-CAS包括一个固体燃料颗粒室，它被点燃以通过喉管排出气体。 排出的气体以大气中的超音速车辆速度被引导到航空控制表面和机身之间的空腔，以对空腔加压并且将其表面或亚音速的速度在大气中或任何速度在外部气氛中流出， 喉部和通孔的表面中的孔提供虚拟的会聚/发散喷嘴以产生超音速转向推力。 没有通孔的颗粒和控制致动系统（P-CAS）在大气中以超音速速度提供命令权限。 限流器机构控制加压气体从空腔排放到外部环境，以实现PT-CAS或P-CAS的部署时间目标。

公开(公告)号：EP2212198A4

公开(公告)日：2016-05-11

申请号：EP08845839

申请日：2008-10-31

Applicant: RAYTHEON CO

Inventor： KINSEY LLOYD E ,  KRANKING PATRICK D

IPC: B64C39/02 ,  B64C29/02

CPC classification number: B64C39/024 ,  B64C29/02 ,  B64C2201/028 ,  B64C2201/084 ,  B64C2201/088