Investigation on Performance Characteristics of Hydrazine Monopropellant Thruster according to Reaction Chamber Adiabatic Temperature
In this paper, by creating and developing a code based on thermodynamics and gas dynamics equations, the performance characteristics of a 1N hydrazine monopropellant thruster such as thrust force, specific impulse, characteristic exhaust velocity, and propellant mass flow rate have been studied theo...
Gorde:
| Egile Nagusiak: | , , , |
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| Formatua: | Artigo |
| Hizkuntza: | Persa |
| Argitaratua: |
Aerospace Research Institute
2022-09-01
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| Saila: | فصلنامه علوم و فناوری فضایی |
| Gaiak: | |
| Sarrera elektronikoa: | https://jsst.ias.ir/article_143736_47f9de12e225fc5dcadaf340f5d9d6d9.pdf |
| Etiketak: |
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