IMPROVED COMPOSITE SOLID PROPELLANTS INCLUDING A HYDROXY-FUNCTIONAL POLYBUTADIENE BINDER AND A ROCKET MOTOR INCLUDING SAME
摘要
Solid propellants for rocket motors contain binders which are hydroxy-functional polybutadiene (HFPB). The HFPB is difunctional and the diene linkages are exclusively 1,4-diene linkages, with no vinyl groups. A rocket motor may contain the solid propellant.
申请公布号
WO0007962(A2)
申请公布日期
2000.02.17
申请号
WO1999US15435
申请日期
1999.07.09
申请人
CORDANT TECHNOLOGIES, INC.
发明人
CANNIZZO, LOUIS, F.;MIDYETT, JEFFREY, S.;HAMILTON, RICHARD, S.
