公开(公告)号：US20240271754A1

公开(公告)日：2024-08-15

申请号：US18168962

申请日：2023-02-14

Applicant: NEOEx Systems, Inc.

Inventor： Mark S. Haberbusch ,  Alec D. Romesberg

IPC: F17C9/00

CPC classification number: F17C9/00 ,  F17C2201/0119 ,  F17C2203/0391 ,  F17C2203/0629 ,  F17C2203/0643 ,  F17C2203/0646 ,  F17C2203/0673 ,  F17C2205/0338 ,  F17C2221/012 ,  F17C2223/0161 ,  F17C2227/0302 ,  F17C2227/0339 ,  F17C2250/04 ,  F17C2270/0189 ,  H01M8/04208

Abstract: An exemplary flight storage system for storing a cryogenic fluid and then discharging it as a vapor. The flight storage system includes an inner tank, a heat exchanger that is in fluid communication with the inner tank, an outer jacket assembly, and a cooling assembly. The storage system is configured to store high specific energy fuel such as liquid hydrogen, or other cryogenic fluids, for energy for propulsion use. The cooling assembly is configured to use the flow of the liquid hydrogen for cooling critical sensor packages The outer jacket assembly includes a first jacket cylinder and a second jacket cylinder. The outer jacket assembly further includes a first connector body 30 and a second connector body.