HYPERGOLIC IGNITION SYSTEM FOR GELLED ROCKET PROPELLANT
摘要
<p>The present invention provides a composition and a system for hypergolic ignition of rocket propellant. The composition includes the suspension of catalytic or reactive particles in a gelled fuel. The catalytic or reactive particles initiate a reaction upon contact with an oxidizer.</p>
申请公布号
WO2011001435(A1)
申请公布日期
2011.01.06
申请号
WO2010IL00527
申请日期
2010.06.30
申请人
TECHNION RESEARCH AND DEVELOPMENT FOUNDATION LTD.;NATAN, BENVENISTE;PERTEGHELLA, VALERIANO;SOLOMON, YAIR
