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
10.08.2021
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2017
|NTIS | 1970
|NTRS | 1983
|Kraftfahrwesen | 1982
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