发明名称 AFT-END IGNITION SYSTEM FOR ROCKET MOTOR
摘要 <p>An igniter for a rocket motor consisting of a cylindrical. tube having an open end and a closed end, a reduced section at the closed end, a plurality of segments extending outwardly from near the closed end, a squib secured in the reduced section, a charge in the tube and a polyurethane foam plug in the open end of the tube.</p>
申请公布号 CA1036419(A) 申请公布日期 1978.08.15
申请号 CA19750234045 申请日期 1975.08.25
申请人 MAJESTY (HER) IN RIGHT OF CANADA AS REPRESENTED BY THE MINISTER OF 发明人 MORRIS, ELIAS P.;CHRISTIE, FRED A.
分类号 C06C9/00;F02K9/95;F42B3/11;F42C19/08;(IPC1-7):42C19/12 主分类号 C06C9/00
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