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U.S. Department of Energy
Office of Scientific and Technical Information

Control of processibility by particle size in high energy solid propellants

Patent ·
OSTI ID:5975654
This patent describes a solid propellant comprised on a weight basis of about 15.15% hydroxyl terminated polybutadiene polymer combined with isophorone diisocyanate. About 0.05% carbon black and about 84.8% of a mixture of unground HMX has an average means diameter of about 150 microns and ground HMX, has an average mean diameter of about 8 - 16 microns, wherein the ratio of the ground to unground HMX is from 60:40 to 70:30 by weight and wherein the composite HMX particle size distribution is within various limits.
Assignee:
Secretary of the Navy, Washington, DC
Patent Number(s):
US 4693764
OSTI ID:
5975654
Country of Publication:
United States
Language:
English