A new system design tool for a hybrid rocket engine-Reference-Cited by-同舟云学术

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A new system design tool for a hybrid rocket engine

Published:2024-10 Issue: Volume:223 Page:119-133
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Quero Granado Elena^ORCID,Hijlkema Jouke^ORCID,Lestrade Jean-Yves^ORCID,Anthoine Jérôme

Funder

ONERA

CNES

Publisher

Elsevier BV

Reference60 articles.

1. Fundamentals of Hybrid Rocket Combustion and Propulsion;Chiaverini,2007

2. Advancing europe’s hybrid rocket engine technology with paraffin and LOX;Schmierer,2019

3. Modeling of high density polyethylene regression rate in the simulation of hybrid rocket flowfields;Bianchi;Aerospace,2019

4. Transient computational thermofluid-dynamic simulation of hybrid rocket internal ballistics;Martino;J. Propuls. Power,2017

5. Three-dimensional numerical modeling of a rocket engine with solid fuel;Kushnirenko;Acta Astronaut.,2021

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