Corrigendum to “Vaporizing liquid microthrusters with integrated heaters and temperature measurement” [Sens. Actuators A 265 (2017) 261–274](S0924424717306490)(10.1016/j.sna.2017.07.032)
Marsil A.C. de Athayde Costa e Silva (TU Delft - Space Systems Egineering)
Daduí Cordeiro Guerrieri (TU Delft - Space Systems Egineering)
H.W. Van van Zeijl (TU Delft - Else Kooi Laboratory, TU Delft - Electronic Components, Technology and Materials)
A Cervone (TU Delft - Space Systems Egineering)
Eberhard K.A. Gill (TU Delft - Space Systems Egineering, TU Delft - Space Engineering)
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Abstract
The authors regret about a mistake in Eq. (2). The correct equation is as follows. [Formula presented]The exit temperature [Formula presented] is the one used to calculate the exit velocity instead of the chamber temperature [Formula presented] as stated in the paper. We assure that the results have been correctly calculated using the correct equation. The authors would like to apologize for any inconvenience caused.
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