Numerical Analysis and Modelling of a 100 N Hypergolic Liquid Bipropellant Thruster

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Advances in Aerospace Science and Technology

ISSN Print: 2473-6708
ISSN Online: 2473-6724
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"Numerical Analysis and Modelling of a 100 N Hypergolic Liquid Bipropellant Thruster"
written by Grace Olileanya Ngwu, Benjamin Iyenagbe Ugheoke, Olatunbosun Tarfa Yusuf, Mopa Ashem Nyabam, Spencer Ojogba Onuh,
published by Advances in Aerospace Science and Technology, Vol.5 No.4, 2020

has been cited by the following article(s):

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[1]	Numerical Analysis of Different Injectors for Kerosene/Hydrogen-Peroxide and Ethanol Amine/Hydrogen-Peroxide for Satellite Thruster
	2024

[2]	Kriyojenik Hidrojen Yakıtlı 100 kN İtki Kapasiteli Bir Roketin RPA Programı ile Kavramsal Tasarım ve Analizi
	Uluslararas? Mühendislik Ara?t?rma ve Geli?tirme Dergisi, 2022

[3]	Metal additive manufacturing for satellites and rockets
	Applied Sciences, 2021

[4]	Preliminary Design, Modelling and Comparison of Green and Toxic Rocket Engines For Kick Stages Applications

[1]	Numerical Analysis of Different Injectors for Kerosene/Hydrogen-Peroxide and Ethanol Amine/Hydrogen-Peroxide for Satellite Thruster SAE Technical Paper Series, 2024 DOI:10.4271/2023-01-5180

[2]	Kriyojenik Hidrojen Yakıtlı 100 kN İtki Kapasiteli Bir Roketin RPA Programı ile Kavramsal Tasarım ve Analizi Uluslararası Muhendislik Arastirma ve Gelistirme Dergisi, 2022 DOI:10.29137/umagd.982713

[3]	Metal Additive Manufacturing for Satellites and Rockets Applied Sciences, 2021 DOI:10.3390/app112412036

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