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- W2079196021 abstract "The thrust produced by a T6 ion engine hollow cathode has been measured using atarget-based system, with argon, krypton and xenon as propellants, for discharge currentvalues of 5-25 A and a wide range of mass flow rates. The calculated values of specificimpulse, which are generally higher for lighter gases, are far in excess of those that could beattributed to heating a gas to thermal equilibrium with the walls. This seems to suggest anarcjet-like operation mechanism." @default.
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- W2079196021 date "2006-07-09" @default.
- W2079196021 modified "2023-09-26" @default.
- W2079196021 title "A Study of the Thrust Generated by a T6 Hollow Cathode" @default.
- W2079196021 cites W2334402657 @default.
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- W2079196021 doi "https://doi.org/10.2514/6.2006-5265" @default.
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