Correction to: Design and Testing of a 3D Printed Regenerative Cooled Nozzle for a Hydrogen Peroxide based Bi-Propellant Thruster (AIAA Propulsion and Energy Forum, 2021)

Correction Notice In the page n°3, in the Hypotheses subsection, the point “The flow can be treated as having infinite thermal capacity” becomes “The exhaust gas flow can be treated as having infinite thermal capacity”. In the page n°5, the equation n°6 q̇vonv,g = ag (Ta − Twg ) becomes q̇conv,g = ag (Twa − Twg ). (a “w” near the “a” is added) In the page n° 21, the Acknowledgments section from: The authors thank Giorgio Massa from Solvay (Rosignano-Livorno, Italy) and Sergey Morozov from Solvay (Brussels, Belgium) for the support and the procurement of Hydrogen Peroxide, Domenico Borrelli and Antonio Caraviello of Sòphia High Tech for manufacturing support, the Industrial Engineering Department and the T4i company for financially supporting the project. Special thanks to T4i technician Alberto Bertipaglia for his dedication and valuable help during the test campaign. becomes: The authors thank Giorgio Massa from Solvay (Rosignano-Livorno, Italy) and Sergey Morozov from Solvay (Brussels, Belgium) for the support and the procurement of Hydrogen Peroxide, Domenico Borrelli and Antonio Caraviello of Sòphia High Tech for manufacturing support. The work of this paper has been partially funded by grant of the ARS01_01181: “PM3-Piattaforma Modulare Multi-Missione” project from Campania Aerospace District (DAC) and by T4i company. Special thanks to T4i technician Alberto Bertipaglia for his dedication and valuable help during the test campaign.