Thermal, Viscosimetric and Thermomechanical Combined Assessment of Mixture Modelled Composite Fuels for Hybrid Propulsion-Reference-Cited by-同舟云学术

Thermal, Viscosimetric and Thermomechanical Combined Assessment of Mixture Modelled Composite Fuels for Hybrid Propulsion

Published:2022-02-21 Issue:4 Volume:47 Page:
ISSN:0721-3115
Container-title:Propellants, Explosives, Pyrotechnics
language:en
Short-container-title:Propellants Explo Pyrotec

Author:

Péres de Araújo Emmanuel¹,José Maschio Leandro²^ORCID,Henrique Gouvêa Leonardo³,Gustavo Ferroni Pereira Luís³,Vieira Ricardo⁴

Affiliation:

1. Department of Chemical Engineering Military Institute of Engineering Rio de Janeiro, RJ Brazil

2. Peroxidos do Brasil Curitiba, PR Brazil

3. Aeronautics Institute of Technology São José dos Campos SP Brazil

4. National Institute for Space Research Cachoeira Paulista, SP Brazil

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202100314

Reference45 articles.

1. G. P. Sutton O. Biblarz Rocket Propulsion Elements John Wiley & Sons Hoboken 2017.

2. Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines

3. Combustion of Liquefying Hybrid Propellants: Part 1, General Theory

4. Combustion of Liquefying Hybrid Propellants: Part 2, Stability of Liquid Films

5. Fuel Regression Rate Characterization Using a Laboratory Scale Nitrous Oxide Hybrid Propulsion System, 42nd AIAA/ASME/SAE/ASEE Jt. Propuls. Conf. Exhib., American Institute Of Aeronautics And Astronautics;Lohner K.;Inc., Sacramento,2006

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