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)

None, None; None, None; None, None; None, None; None, None

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)

Author(s)

Marsil A.C. Silva (TU Delft - Aerospace Engineering)

Daduí C. Guerrieri (TU Delft - Aerospace Engineering)

Henk van Zeijl (TU Delft - Electrical Engineering, Mathematics and Computer Science, TU Delft - Electrical Engineering, Mathematics and Computer Science)

Angelo Cervone (TU Delft - Aerospace Engineering)

Eberhard Gill (TU Delft - Aerospace Engineering, TU Delft - Aerospace Engineering)

Research Group

Space Systems Egineering

DOI related publication

https://doi.org/10.1016/j.sna.2018.05.004 Final published version

To reference this document use

https://resolver.tudelft.nl/uuid:ee985d6e-53f7-4028-8866-938f3df7b93a

More Info

expand_more

Publication Year

2018

Language

English

Research Group

Space Systems Egineering

Journal title

Sensors and Actuators, A: Physical

Volume number

277

Downloads counter

168

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.