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)

Journal article (2018)

Authors

M. de Athayde Costa e Silva Space Systems Egineering
D. Cordeiro Guerrieri Space Systems Egineering
H.W. van Zeijl Electronic Components, Technology and Materials - EEMCS , Else Kooi Laboratory
A. Cervone Space Systems Egineering
E.K.A. Gill Space Systems Egineering , Space Engineering
Research Group
Space Systems Egineering
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Published Date

01-07-2018

Language

English

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Research Group

Space Systems Egineering

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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