F17C5/002

SPACE ELECTRIC PROPULSION SYSTEM AND XENON FILLING METHOD THEREFOR
20260077884 · 2026-03-19 ·

A space electric propulsion system and a xenon filling method therefor are provided, suitable for a filling process of an electric propulsion system using high-purity xenon as a working medium. By reasonably designing a filling process, the precision of a xenon filling amount is ensured, and xenon filling can be performed without weighing the whole spacecraft. This method features a simple and efficient filling device, short preparation time, precise and controllable filling process, as well as safety and convenience, which can effectively meet the requirements for a high-purity xenon rapid filling task of a satellite.

CRYOGEN FILLING APPARATUS

A fill control system and method are provided. The system may include valves connecting a cryogen vessel to a cryogen manifold. The system may detect a cooling of the cryogen manifold caused by filling of another cryogen vessel with cryogen, and responsively initiate its own filling process. Thus, a number and duration of venting instances is reduced. Before filling a cryogen vessel with cryogen, a fill control system may vent filling lines and/or a cryogen manifold to limit introduction of warm fluid into a cryogen vessel. By determining when another fill control system has already initiated venting of the cryogen manifold (indicated by cooling of the cryogen manifold as cryogen flows), a fill control system reduces the amount of venting that it must perform prior to filling its associated cryogen vessel from the cryogen manifold.

INTENTIONALLY CHOKED FLOW DURING AN INITIAL PHASE OF A COMPRESSIBLE FLUID FILLING OPERATION
20260132890 · 2026-05-14 ·

A system includes a storage tank and a feed line that supplies a compressible fluid from a high-pressure source to a plurality of fluid lines in fluid communication with the storage tank. The plurality of fluid lines includes a first fluid line having a first inner diameter sized to create choked flow conditions of the compressible fluid in the first fluid line at an outlet of the first fluid line and a second fluid line having a second inner diameter greater than the first inner diameter. The system further includes a first valve in fluid communication with the second fluid line and a control circuit in electronic communication with the first valve. The control circuit actuates the first valve to control a flow of the compressible fluid through an outlet of the second fluid line.