Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection-Reference-Cited by-同舟云学术

Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection

Published:2023-09 Issue: Volume:140 Page:108467
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Migliorino Mario Tindaro^ORCID,Fabiani Marco^ORCID,Paravan Christian^ORCID,Bianchi Daniele^ORCID,Nasuti Francesco^ORCID,Galfetti Luciano,Pellegrini Rocco Carmine^ORCID,Cavallini Enrico^ORCID

Funder

Agenzia Spaziale Italiana

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference68 articles.

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3. Approaches to low fuel regression rate in hybrid rocket engines;Pastrone;Int. J. Aerosp. Eng.,2012

4. Recent advances in hybrid propulsion;Cantwell;Int. J. Energ. Mater. Chem. Propuls.,2010

5. Advancing Europe's hybrid rocket engine technology with paraffin and LOX;Schmierer,2019

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