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    MODULARE FESTSTOFFRAKETENTREIBSÄTZE MIT UMMANTELUNG, FILL-DRAIN SYSTEM, KÜHLUNG UND AUFHÄNGUNG
    4.
    发明公开
    MODULARE FESTSTOFFRAKETENTREIBSÄTZE MIT UMMANTELUNG, FILL-DRAIN SYSTEM, KÜHLUNG UND AUFHÄNGUNG 有权
    与环绕模块化固体火箭DRIVE套件，填漏系统，冷却和暂停

    公开(公告)号：EP1080302A1

    公开(公告)日：2001-03-07

    申请号：EP99936294.0

    申请日：1999-05-18

    申请人： Lo, Roger E.

    发明人： Lo, Roger E.

    IPC分类号： F02K9/10 ,  F02K9/34 ,  F02K9/40 ,  F02K9/36 ,  C06B45/00

    CPC分类号： F02K9/40 ,  F02K9/00 ,  F02K9/10 ,  F02K9/32 ,  F02K9/36

    摘要： The invention relates to modular solid-fuel rocket propelling charges comprising different propellant components and other components, for example, fuels, oxidators, energy increasing admixtures, binders, additives, coatings, inhibitors, etc. which can be completely or partially fragmented, i.e. they are not provided in the form of the conventional quasi homogeneous mixture, rather they are available in the form of one or more macroscopic combustible elements having any appropriate configuration. All or individual components can also be comprised of substances which must first be sufficiently brought to a solid state by cooling. The aim of the invention is to provide modular solid-fuel rocket propelling charges of the aforementioned type such that the development of dangerous situations resulting from a cooling failure during simultaneous power increases of the carrier rockets is drastically minimized. To this end, the modules are provided as an assembly or the individual combustible elements thereof are provided with a special casing (1). Said special casing permits the storage of such propelling charges and/or the operation thereof according to prescription in such a way that problems do not occur due to the dependence on temperature of the mechanical characteristics or of the state of the aggregate.

    Aménagement interne anti-clappement pour propulseur à poudre et son procédé de fabrication
    5.
    发明公开
    Aménagement interne anti-clappement pour propulseur à poudre et son procédé de fabrication 失效
    设备和生产中的固体燃料火箭内部应力释放。

    公开(公告)号：EP0226499A1

    公开(公告)日：1987-06-24

    申请号：EP86402573.9

    申请日：1986-11-20

    申请人： SOCIETE EUROPEENNE DE PROPULSION

    发明人： Beboux, Jean

    IPC分类号： F02K9/36 ,  F02K9/34

    CPC分类号： F02K9/36 ,  F02K9/346

    摘要： Un bloc de poudre (11) est logé dans une enveloppe (10) avec interposition d'une protection thermique (12) et délimite une chambre de combustion (13), un décollement (15, 20) est formé entre le bloc de poudre (11) et le revêtement (17, 22) de protection thermique de la structure de fond du propulseur au moyen d'une peau (16, 21) décollée dudit revêtement et adhérant au bloc de poudre, au moins une des deux parties que constituent la peau décollée (16, 21) et le revêtement (17, 22) de protection thermique de la structure de fond du propulseur présentant des protubérances ou picots (18, 23)) pour assurer un écartement minimum de la peau décollée par rapport audit revêtement et faciliter l'accès des gaz dans le décollement (15, 20).

    PELLET LOADED ATTITUDE CONTROL ROCKET MOTOR
    7.
    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.

    MODULARE FESTSTOFFRAKETENTREIBSÄTZE MIT UMMANTELUNG, FILL-DRAIN SYSTEM, KÜHLUNG UND AUFHÄNGUNG
    8.
    发明授权
    MODULARE FESTSTOFFRAKETENTREIBSÄTZE MIT UMMANTELUNG, FILL-DRAIN SYSTEM, KÜHLUNG UND AUFHÄNGUNG 有权
    与环绕模块化固体火箭DRIVE套件，填漏系统，冷却和暂停

    公开(公告)号：EP1080302B1

    公开(公告)日：2002-07-03

    申请号：EP99936294.0

    申请日：1999-05-18

    申请人： Lo, Roger E.

    发明人： Lo, Roger E.

    IPC分类号： F02K9/10 ,  F02K9/34 ,  F02K9/40 ,  F02K9/36 ,  C06B45/00

    CPC分类号： F02K9/40 ,  F02K9/00 ,  F02K9/10 ,  F02K9/32 ,  F02K9/36

    摘要： The invention relates to modular solid-fuel rocket propelling charges comprising different propellant components and other components, for example, fuels, oxidators, energy increasing admixtures, binders, additives, coatings, inhibitors, etc. which can be completely or partially fragmented, i.e. they are not provided in the form of the conventional quasi homogeneous mixture, rather they are available in the form of one or more macroscopic combustible elements having any appropriate configuration. All or individual components can also be comprised of substances which must first be sufficiently brought to a solid state by cooling. The aim of the invention is to provide modular solid-fuel rocket propelling charges of the aforementioned type such that the development of dangerous situations resulting from a cooling failure during simultaneous power increases of the carrier rockets is drastically minimized. To this end, the modules are provided as an assembly or the individual combustible elements thereof are provided with a special casing (1). Said special casing permits the storage of such propelling charges and/or the operation thereof according to prescription in such a way that problems do not occur due to the dependence on temperature of the mechanical characteristics or of the state of the aggregate.