公开(公告)号：US3582413A

公开(公告)日：1971-06-01

申请号：US3582413D

申请日：1963-02-15

Applicant: US ARMY

Inventor： ALLAN BARRY D ,  CONNAUGHTON JOSEPH W

IPC: C06B23/00 ,  C06B43/00 ,  C06D5/00

CPC classification number: C06B23/007 ,  C06B43/00 ,  Y10S149/122

Abstract: 1. IN LIQUID ROCKET ENGINES UTILIZING AS A PROPELLANT COMPONENT A DIFLUOROAMINO DERIVATIVE OF THE FORMULA

F2N-C(-A)(-Z)-C(-X)(-Y)-NF2

WHEREIN A, Z, X, AND Y ARE EACH A MEMBER SELECTED FROM THE GROUP CONSISTING OF HYDROGEN AND LOWER ALKYL GROUPS OF UP TO FOUR CARBON ATOMS, THE TOTAL NUMBER OF CARBON ATOMS IN A, Z, X, AND Y NOT TO EXCEED SIX, THE IMPROVEMENT WHICH COMPRISES INCORPORATING IN SAID DIFLUOROAMINO DERIVATIVES AS A BURNING RATE MODIFIER A SUFFICIENT AMOUNT OF A MEMBER SELECTED FROM THE GROUP CONSISTING OF FERRIC CHLORIDE, ZINC CHLORIDE, AND STANNOUS CHLORIDE TO FORM A SATURATED SOLUTION THEREOF.