Cryogenic solid hybrid rocket engine and method of propelling a

Power plants – Reaction motor – Solid and fluid propellant

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60204, F02K 928

Patent

active

061018082

ABSTRACT:
A cryogenic solid hybrid engine with a solid propellant chamber, a first propellant within such chamber in which the first propellant is in solid form in the chamber and is in fluid form at room temperature, a coolant fluid chamber and a coolant fluid in the coolant fluid chamber being maintained at a temperature blow the freezing point of the first propellant. The invention also relates to a method for propelling a rocket and a method for forming a solid propellant grain for use in a cryogenic solid hybrid rocket engine.

REFERENCES:
patent: 5099645 (1992-03-01), Schuler et al.

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