Aerojet Rocketdyne of De, Inc.

Hamilton Sundstrand Space Systems International, Inc.

Cheng-Yi Lu

William Determan

Kenneth John Metcalf

Rick L Howerton

Andrew J Zillmer

Joseph P Carroll

Gregory A Johnson

Patrick Edward Frye

Erich H Soendker

David Wait

Brian M Sutin

James A McClanahan

David Grimmett

Marcelo Bromberg

Charles Thomas Kudija

A power converter is provided and includes a heat collector surface, n- and p-legs formed of n- and p-type thermoelectric materials, respectively, which are each disposed in thermal communication with the heat collector surface, parallel electric busses electrically coupled to the n- and p-legs and a housing, which is electrically decoupled from the busses, to support the heat collector surface at a predefined distance from a heat pipe.

Power converter

A heat rejection system includes a plurality of panel subassemblies and a solid state heat pipe flex joint. Each panel subassembly includes a fin, a solid state heat pipe manifold, a first solid state heat pipe tube operatively connected to the solid state heat pipe manifold and secured to the fin, a second solid state heat pipe tube operatively connected to the solid state heat pipe manifold adjacent to the first solid state heat pipe and secured to the fin. The solid state heat pipe flex joint operably connects the solid state heat pipe manifolds of two of the plurality of panel subassemblies in a hermetically sealed configuration, and is configured to permit repositioning of the two panel subassemblies relative to each other.

Solid state heat pipe heat rejection system for space power systems

A center-tapped solar array includes a plurality of series-connected solar cells connected between a positive terminal and a negative terminal for generating an output voltage. A center-tapped terminal connected to ground is connected to the plurality of series-connected solar cells at a midpoint between the positive and negative terminals. As a result, the positive terminal of the solar array has a positive voltage relative to ground greater than the center-tapped terminal and the negative terminal has a negative voltage relative to ground less than the center-tapped terminal.

Center-tapped solar array and power distribution system for same

A rechargeable battery assembly provides load balancing for individual battery cells making up a battery assembly. The battery assembly includes a plurality of series-connected battery cell assemblies. Each battery cell assembly includes a battery cell and a charge bypass load connected in parallel with the battery cell. A cell supervisory circuits (CSCs) and battery interface unit (BUI) interface between the battery cell assembly and a battery charge/discharge circuit to provide load balancing by comparing the voltages monitored with respect to each battery cell assembly to an end of charge voltage (EOCV) threshold and in response to the monitored voltage equaling the EOCV threshold issues a charge bypass command to the CSC to activate the charge bypass load.

Charge balancing topology

A solar receiver device includes a metal conduit and a glass container disposed around the metal conduit such that there is a space between the glass container and the conduit. A coating is disposed on the metal conduit and has a composition that includes at least one element from silicon, titanium, aluminum, barium, and samarium.

Solar receiver and solar power system having coated conduit

An apparatus is provided and includes a reactor core, a boom and a shield assembly supportively interposed between the reactor core and the boom, a heat pipe disposed in thermal communication with the reactor core, a thermoelectric power converter operably coupled to the heat pipe, struts supportively coupled to the heat pipe at opposite ends of the power converter and hinge joints to rotatably couple the struts to the boom, at least one of the hinge joints being spring-loaded.

Thermoelectric power converter support structure

An example space-based power generation panel arrangement includes a first reflective panel and at least one heat pipe configured to communicate thermal energy to the first reflective panel and a second reflective panel. The heat pipe is configured to hinge the first reflective panel to the second reflective panel.

Growing community of inventors

West Hills, CA, United States of America

Cheng-Yi Lu