发明名称 Pellet-loaded multiple impulse rocket motor
摘要 There is disclosed an apparatus which may include a common nozzle and a plurality of combustion chambers coupled to the nozzle. Each of the plurality of combustion chambers may include a case, a solid fuel propellant charge in the form of a plurality of fuel pellets, and an igniter disposed to ignite the propellant charge. Each of the plurality of combustion chambers may also include a pellet retainer disposed to retain unignited fuel pellets within the case and a burst disk disposed between the propellant charge and the nozzle. Each burst disk may adapted to rupture when the associated propellant charge is ignited and to not rupture when a propellant charge of any of the other combustion chambers is ignited.
申请公布号 US8667776(B2) 申请公布日期 2014.03.11
申请号 US20090391216 申请日期 2009.02.23
申请人 OLDEN THOMAS A.;CAVALLERI ROBERT J.;RAYTHEON COMPANY 发明人 OLDEN THOMAS A.;CAVALLERI ROBERT J.
分类号 F02K9/28;F02K9/00 主分类号 F02K9/28
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