发明名称 Solid propellant rocket motor with notched annular fuel
摘要 A motor includes an annular solid fuel between an inside diameter and an outside diameter. The solid fuel has a series of radial notches that define segments of fuel between them. The notches allow for faster burning of the fuel, while still allowing structural integrity of the fuel segments to be retained during the burning process.
申请公布号 US8181444(B2) 申请公布日期 2012.05.22
申请号 US20080240223 申请日期 2008.09.29
申请人 DUPONT JAMES H.;LOEHR RICHARD D.;RENZ ROBERT N.;RAYTHEON COMPANY 发明人 DUPONT JAMES H.;LOEHR RICHARD D.;RENZ ROBERT N.
分类号 F02K9/00 主分类号 F02K9/00
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