Solid fuel ramjet composition
First Claim
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1. A solid ramjet fuel consisting essentially of hydroxyl terminated polybutadiene, magnesium and boron carbide wherein the weight percentages of said fuel are from 5-35% Mg, from 30-35% B4 C and from 30-65% HTPB.
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Abstract
A ramjet solid fuel composed of Hydroxyl terminated polybutadiene aluminum,agnesium, and boron carbide is described. The high volumetric heating value fuel of the present invention significantly increases the distance range of missiles.
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3 Claims
- 1. A solid ramjet fuel consisting essentially of hydroxyl terminated polybutadiene, magnesium and boron carbide wherein the weight percentages of said fuel are from 5-35% Mg, from 30-35% B4 C and from 30-65% HTPB.
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3. A solid ramjet fuel consisting essentially of hydroxyl terminated polybutadiene (HTPB), magnesium, aluminum and boron carbide wherein the weight percentages of said fuel are about 10% magnesium, about 15% aluminum, about 25% boron carbide and about 50% HTPB.
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Current Assigneethe united states of america as represented by the secretary of the navy
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Original Assigneethe united states of america as represented by the secretary of the navy
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InventorsMeyers, Gary W., Burdette, George W.
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Primary Examiner(s)Miller, Edward A.
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Application NumberUS06/329,621Time in Patent Office4,584 DaysField of Search60/207, 149/19.2, 149/19.9, 149/87US Class Current149/19.9CPC Class CodesC06B 45/10 the organic component conta...C06D 5/00 Generation of pressure gas,...
