초록 ▼

Ergols, particularly for propelling missiles, containing at least one oxidant, a fuel and an energy-releasing binder. The oxidant is selected from the group which includes a nitroformate of a nitrogen compound, particularly hydrazinium or ammonium nitroformate, and a perchlorate of a nitrogen compou

Ergols, particularly for propelling missiles, containing at least one oxidant, a fuel and an energy-releasing binder. The oxidant is selected from the group which includes a nitroformate of a nitrogen compound, particularly hydrazinium or ammonium nitroformate, and a perchlorate of a nitrogen compound, particularly nitronium or ammonium perchlorate. The fuel is selected from the group which includes boron and boranes, aluminium and aluminium hydribe. The energy-releasing binder is selected from the group which includes polyglycidyl nitrate, polyglycidyl azide, polynitromethoxymethyloxetane and poly-3,3bis(azidomethyl)oxetane. Said ergols are particularly useful for propelling aerospace missiles, particularly rockets.

대표청구항 ▼

[ We claim:] [1.] A solid propellant for the propulsion of aerospace vehicles comprising at least an oxidizer, a fuel and an energetic binder;wherein the oxidizer is ammonium nitroformate;wherein the fuel is selected from the group consisting of boron, aluminum and aluminum hydride; andwherein the e

[ We claim:] [1.] A solid propellant for the propulsion of aerospace vehicles comprising at least an oxidizer, a fuel and an energetic binder;wherein the oxidizer is ammonium nitroformate;wherein the fuel is selected from the group consisting of boron, aluminum and aluminum hydride; andwherein the energetic binder is selected from the group consisting of polyglycidyl nitrate, and polynitromethoxymethyloxetane.