A quick disconnect apparatus including a first end configured to interface with a legacy fill and drain valve (FDV) of a satellite to be serviced, a second end configured to interface with a refueling tool, and a middle portion including at least one redundant seal to prevent unwanted fuel transfer during connection of the FDV and refueling tool.
Refueling tool and quick disconnect
2021-08-10
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2017
|NTRS | 1983
|Kraftfahrwesen | 1982
|Europäisches Patentamt | 2019
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