Power plants – Reaction motor – Turborocket
Reexamination Certificate
2005-10-11
2005-10-11
Nguyen, Hoang (Department: 3748)
Power plants
Reaction motor
Turborocket
C060S251000
Reexamination Certificate
active
06952917
ABSTRACT:
The engine for a rocket is suitable for using for an educational program. The engine uses a liquid phase propellant having a predetermined boiling point and a heating substance having a temperature higher than the boiling point. The engine has an inner wall having a circumferential surface; an outer wall surrounding the inner wall, the outer wall having an interior surface spaced from the circumferential surface of the inner wall by a predetermined distance such that the space between the circumferential surface and the interior surface form a mixing chamber having an opening; and injector for injecting the liquid-phase propellant and the heating substance into the mixing chamber so that the propellant is evaporated by the heating substance thereby creating a jet stream moving from the opening of the mixing chamber to the outside of the mixing chamber.
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E.V. Mukerjee et al., “Vaporizing liquid microthruster,”Sensors and Actuators A, vol. 83, No. 1-3 (Elseviier Sequoia S.A., Lausanne, Switzerland, May 2000), pp. 231-236.
Japan Aerospace Exploration Agency
Nguyen Hoang
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