Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer

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Edalatpour Amirhossein; Ommi Fatholah; SABOOHI ZOHEIR

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Journal Paper

Paper Information

Journal: Journal of Space Science and Technology Year:2019 | Volume:12 | Issue:1 (38) Page(s): 23-40

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Title

Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer

Author(s)

Edalatpour Amirhossein | Ommi Fatholah | SABOOHI ZOHEIR | Issue Writer Certificate

Keywords

micro-propulsionQ1

cryogenic oxidizerQ1

injectorQ2

combustion chamberQ2

nozzleQ1

heat transferQ2

hot fire testQ1

Abstract

micro-propulsion Systems are low thrust engines that be used in space missions like keeping satellite in orbit and changing orbit. These engines have several kinds and liquid propellant micro-propulsion is used in this project. In two propellant micro-propulsion systems, various fuels and oxidizers can be used. Kerosene is used as fuel and liquid oxygen is used as oxidizer in this project. First of all, a micro-propulsion is designed and analysis of combustion, heat transfer, nozzle exit flow and amount of performance’ s parameters is done with RPA software. Similar to big engines, micro-propulsion systems have injectors, injection plate, combustion chamber and nozzle. Design of all of this parts will be explained. With manufacturing of designed model and perform hot fire test, accurate performance of engine is observed. Finally, performance’ s parameters in hot fire test are compared with performance’ s parameters in RPA.

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APA: Copy

Edalatpour, Amirhossein, Ommi, Fatholah, & SABOOHI, ZOHEIR. (2019). Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 12(1 (38) ), 23-40. SID. https://sid.ir/paper/400313/en

Vancouver: Copy

Edalatpour Amirhossein, Ommi Fatholah, SABOOHI ZOHEIR. Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2019;12(1 (38) ):23-40. Available from: https://sid.ir/paper/400313/en

IEEE: Copy

Amirhossein Edalatpour, Fatholah Ommi, and ZOHEIR SABOOHI, “Performance Analysis of Liquid Propellant Micro-propulsion with Liquid Oxygen as Cryogenic Oxidizer,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 12, no. 1 (38) , pp. 23–40, 2019, [Online]. Available: https://sid.ir/paper/400313/en

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