Experimental investigation of the axial oxidizer injectors geometry on a 1-kN paraffin-fueled hybrid rocket motor-Reference-Cited by-同舟云学术

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Experimental investigation of the axial oxidizer injectors geometry on a 1-kN paraffin-fueled hybrid rocket motor

Published:2021-12 Issue:4 Volume:1 Page:231-243
ISSN:2667-1344
Container-title:FirePhysChem
language:en
Short-container-title:FirePhysChem

Author:

Bouziane M.,Bertoldi A.E.M.,Hendrick P.,Lefebvre M.

Publisher

Elsevier BV

Reference26 articles.

1. Numerical modeling of self-pressurizing oxidizers for hybrid rocket injection;Invigorito,2015

2. Overview and history of hybrid rocket propulsion;Altman;Prog. Astronaut. Aeronaut.,2007

3. Rocket Propulsion Elements;Sutton,2016

4. Transient analysis on ignition process of catalytic hybrid rocket motor;Cai;Aerosp. Sci. Technol.,2017

5. Trade-off between paraffin-based and aluminium-loaded HTPB fuels to improve performance of hybrid rocket fed with N2O;Carmicino;Aerosp. Sci. Technol.,2014

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Multiphysics Modeling for Combustion Instability in Paraffin-Fueled Hybrid Rocket Engines;Journal of Spacecraft and Rockets;2024-05

2. Experimental test analysis of a 300 N hybrid rocket engine;Aerospace Systems;2024-01-19

3. Test Activities on Hybrid Rocket Engines: Combustion Analyses and Green Storable Oxidizers—A Short Review;Aerospace;2023-06-21

4. Numerical study of the effect of fuel droplets on the combustion proceeding under typical conditions of hybrid rocket engines;Thermophysics and Aeromechanics;2023-06-05

5. 3D Printing Techniques for Paraffin-Based Fuel Grains;Aerotecnica Missili & Spazio;2022-09

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