Back to results
US 4,302,258 AGranted
Composite propellant with 0.2.mu. or smaller metal fuel
AssigneeNissan Motor Co., Ltd.
InventorsDaizo Fukuma, Hisao Okamoto, Sumio Okamoto, Takemasa Koreki
Life of this patent
Estimating the term…
Abstract
A composite-type propellant is disclosed. The propellant contains metal grains having an average grain size of not more than 0.2.mu. as an exothermic agent.
Claims6
A composite-type propellant comprising metal grains as an exothermic agent, an oxidizing agent, a fuel binder and a catalyst, wherein the average size of said metal grains is not more than 0.2.mu., and is selected to provide a propellant slurry viscosity during manufacture not greater than about 30,000 poise.
Dependencies are inferred from the claim text.