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US 2018/0273439 A1Published application
Solid rocket propellant with blended triazole plasticzer
AssigneeAerojet Rocketdyne, Inc.
InventorScott DAWLEY
Life of this patent
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Abstract
A solid rocket propellant includes a blended plasticizer of at least two chemically different 3-nitro 1,2,4-triazoles.
Claims18
A solid rocket propellant comprising a blended plasticizer of at least two chemically different 3-nitro 1,2,4-triazoles.
A solid rocket motor comprising:
- a motor case;
- a nozzle attached with the motor case;
- and
- a solid rocket propellant disposed in the motor case, the solid rocket propellant including a blended plasticizer of at least two chemically different 3-nitro 1,2,4-triazoles.
1 more element
A solid rocket propellant comprising a blended triazole plasticizer with a density from 1.51 grams per cubic centimeter to 1.63 grams per cubic centimeter, and a glass transition temperature of −62° C. to −75° C.
Dependencies are inferred from the claim text.