USA As Represented by Secretary of the Navy

Robert W Baldauff

Triem T Hoang

Jesse R Maxwell

Dmitry Khrustalev

Adam Thurn

Timothy Holman

Kwok Cheung

Gabriel B Goodwin

Ronald L Sutton

Stephen M Koss

Evan Hyde

Philip A Feerst

A pump-augmented Loop Heat Pipe (LHP) includes a conventional LHP evaporator/reservoir assembly; one or more additional evaporators; a condenser; a condenser bypass; and a pump upstream of the condenser and condenser bypass and configured to pump fluid generally toward the one or more additional evaporators.

Architecture and operational modes of pump-augmented loop heat pipe with multiple evaporators

A hybrid capillary and mechanically pumped loop heat pipe (HLHP) includes a fluid loop having an evaporator thermally coupled to a heat load, a condenser thermally coupled to a heat sink, a reservoir, and one or more magnetically levitating pumps configured to pump fluid through the loop thereby improving heat transport capacity and system stability.

Hybrid loop heat pipe with integrated magnetically levitating bearingless pump

A method of thermally protecting a leading edge of a hypersonic system includes saturating an annular primary wick in contact with an evaporator and having a first pore size with a phase change material by means of an annularly-inward secondary wick having a second pore size and being coupled to a liquid line, the second pore size being larger than the first, where a first end of the secondary wick extends into a reservoir and a second end of the secondary wick extends into the evaporator, the second end of the secondary wick having a terminal end. The method includes terminating the liquid line inside of the evaporator, transferring thermal energy from the leading edge into the phase change material, raising the temperature of the phase change material to a phase-change temperature, changing phase of the phase change material, and carrying away heat from the leading edge.

Two-phase thermal protection of the hypersonic leading edge

A twist capsule rotary joint system for passing a fluid through a pressure hull without a dynamic seal. A rotating cylindrical drum positioned outboard of the pressure hull is adapted to be driven in a reciprocating manner through an angle and backward through the same angle. At least one outboard pressure line or hose has a first end attached to a fixed connector that extends through the pressure hull near and radially outward of the rotating cylindrical drum. A second end of the outboard pressure line or hose is attached to a connector that extends through the top outboard surface of the drum. As the drum rotates, the pressure line wraps around the drum, or unwraps from the drum. In an exemplary embodiment, two pressure lines carry two-phase coolant through the pressure hull of a spacecraft in support of a rotating radiator that is adapted to rotate to present a minimum surface area toward the sun.

Flexible pressure line twist capsule rotary union for steerable spacecraft radiator

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Mechanicsville, MD, United States of America

Robert W Baldauff