Abstract: Example implementations relate to techniques for thermal fluid conditioning and delivery. A technique may involve coupling a container of heat transfer fluid to an input and removing moisture from the heat transfer fluid via a molecular sieve. A pressure source is configured to push the heat transfer fluid out of the container and through the molecular sieve. Subsequent to removing the moisture from the heat transfer fluid, the technique involves separating, via an orifice coupled to a tank, the heat transfer fluid into liquid and gas particles within the tank and removing, via a vacuum coupled to the tank, the gas particles from the tank. The liquid can then be supplied into a fluid system via additional pressure by the pressure source. The technique may be performed by a portable device that houses the various components used to condition and delivery the thermal fluid.

Abstract: The present application relates to systems, methods, and apparatus for facilitating the testing of a payload. An exemplary apparatus may include a fluid inlet port configured to receive fluid from a thermal subsystem of the payload. The apparatus may also include an actuating device configure to supply the fluid to a heat exchanger. A valve may be configured to receive the fluid from the heat exchanger and separate the fluid into a first fluid line and a second fluid line. A first fluid outlet port may be configured to supply the fluid to the thermal subsystem of the payload and a second fluid outlet port may be configured to supply the fluid to the thermal subsystem of payload.

Abstract: The present application relates to systems, methods, and apparatus for facilitating the testing of a payload. An exemplary apparatus may include a fluid inlet port configured to receive fluid from a thermal subsystem of the payload. The apparatus may also include an actuating device configure to supply the fluid to a heat exchanger. A valve may be configured to receive the fluid from the heat exchanger and separate the fluid into a first fluid line and a second fluid line. A first fluid outlet port may be configured to supply the fluid to the thermal subsystem of the payload and a second fluid outlet port may be configured to supply the fluid to the thermal subsystem of payload.

Abstract: Example implementations relate to techniques for thermal fluid conditioning and delivery. A technique may involve coupling a container of heat transfer fluid to an input and removing moisture from the heat transfer fluid via a molecular sieve. A pressure source is configured to push the heat transfer fluid out of the container and through the molecular sieve. Subsequent to removing the moisture from the heat transfer fluid, the technique involves separating, via an orifice coupled to a tank, the heat transfer fluid into liquid and gas particles within the tank and removing, via a vacuum coupled to the tank, the gas particles from the tank. The liquid can then be supplied into a fluid system via additional pressure by the pressure source. The technique may be performed by a portable device that houses the various components used to condition and delivery the thermal fluid.

Abstract: A space vehicle is described. The space vehicle comprises one or more heat-producing components, and a closed loop cooling system configured to remove heat generated by the one or more heat-producing components. The closed loop cooling system comprises a coolant passageway defining a closed loop, a coolant located within the coolant passageway, the coolant comprising a static pressure of 100 pounds per square inch or lower and the coolant being in a single liquid phase through the coolant passageway, and one or more pumps configured to move the coolant through the coolant passageway. The closed loop cooling system further comprises a first heat exchange component disposed along the coolant passageway, the first heat exchange component configured to transfer heat from the heat-producing components to the coolant, and a second heat exchange component disposed along the coolant passageway, the second heat exchange component configured to remove heat from the coolant.

Abstract: In one aspect a satellite comprises a body, a solid state power amplifier, a heat acquisition and transfer device positioned proximate at least one heat generating element on the solid state power amplifier, and a heat rejection device in thermal communication with the heat acquisition and transfer device to reject heat acquired from the solid state power amplifier. Other aspects may be described.

Abstract: In one aspect a satellite comprises a body, a solid state power amplifier, a heat acquisition and transfer device positioned proximate at least one heat generating element on the solid state power amplifier, and a heat rejection device in thermal communication with the heat acquisition and transfer device to reject heat acquired from the solid state power amplifier. Other aspects may be described.