Propellant transfer system and method for resupply of fluid propellant to on-orbit spacecraft
US9260206B2 · kind B2 · utility
12Cited by
26References
11Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 26, 2014 |
| Grant date | Feb 16, 2016 |
| Priority date | — |
| Expiry date | Feb 7, 2035 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64G2004/005
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
Herein is disclosed a propellant transfer system and method for refueling on-orbit spacecraft. The system and method are configured to allow for resupply of spacecraft configured to be fueled by either a bipropellant (oxidizer and fuel) or a monopropellant (typically hydrazine). The system and method are particularly suited for resupply of satellites not originally prepared for refueling as well but the system may also be used for as satellites specifically designed for refueling.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.