Physical Configuration Design of a 10N Monopropellant Hydrazine Thruster [PDF]
فصلنامه علوم و فناوری فضایی, 2019 In this paper, design and physical configuration of various components of a 10N Monopropellant Hydrazine Thruster focusing on design calculations and optimization of catalytic combustion chamber. According to this design, a prototype of the thruster will
Hadiseh Karimaei +3 more
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Geometrical characterization and performance optimization of monopropellant thruster injector
Egyptian Journal of Remote Sensing and Space Sciences, 2012 The function of the injector in a monopropellant thruster is to atomize the liquid hydrazine and to distribute it over the catalyst bed as uniformly as possible. A second objective is to place the maximum amount of catalyst in contact with the propellant
T.R. Nada, A.A. Hashem
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Experimental Investigation of a Monopropellant Thruster Using Nitrous Oxide
Journal of Aerospace Technology and Management, 2014 Nitrous oxide is a monopropellant with potential for use in propulsion systems for orbit correction, positioning and attitude control of satellites.
Luciano Hennemann +2 more
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Pulse-mode Performance Evaluation of a Monopropellant Hydrazine Thruster [PDF]
علوم، فناوری و کاربردهای فضایی, 2023 In this study, the pulse mode performance of a monopropellant hydrazine thruster has been studied. For this purpose, a laboratory sample of a monopropellant hydrazine thruster under atmospheric pressure was fabricated and tested.
mohamad ali amirifar +3 more
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Design and Configuration of Ground Sample Components of Low Propulsion Monopropellant Thruster Using Some Engineering Software [PDF]
فصلنامه علوم و فناوری فضایی, 2021 Monopropellant thruster are used to inject a satellite into orbit or control its position on three axes in space missions. One of them is hydrazine thruster which is widely used.
Sajjad Davari +3 more
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Optimized Dimension Design of Catalytic Chamber of a 10 N Thruster [PDF]
فصلنامه علوم و فناوری فضایی, 2023 In this paper, the catalyst bed of a 10 N hydrazine monopropellant thruster was designed. The catalyst bed is including iridium granules, which is used to decompose the hydrazine in monopropellant thruster.
Sajjad Davari +3 more
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Design and Simulation of Single Capillary Injector and Circular Injector Plate for a Monopropellant Thruster [PDF]
فصلنامه علوم و فناوری فضایی, 2022 In this research, design and simulation of a single capillary injector and three-hole circular injector plate of a 10N Hydrazine monopropellant thruster were performed. Ansys Fluent software was used to simulate the injector and injector plate .
Sajad Davari, Hadiseh Karimaei
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Investigation on Performance Characteristics of Hydrazine Monopropellant Thruster according to Reaction Chamber Adiabatic Temperature [PDF]
فصلنامه علوم و فناوری فضایی, 2022 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 ...
Seyyed Rashad Rouholamini +3 more
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Experimental Investigation of the Performance of a Monopropellant Hydrazine Thruster in Atmospheric Conditions [PDF]
علوم، فناوری و کاربردهای فضایی, 2022 In this research, the performance of a monopropellant hydrazine thruster in atmospheric conditions has been investigated experimentally. For this purpose, after designing and constructing the thruster according to the functional requirements of the ...
mohamad ali amirifar +4 more
doaj +1 more source
Study the Performance of Hydrazine Monopropellant Thruster Catalysts with Different Iridium Loading [PDF]
علوم، فناوری و کاربردهای فضایی, 2022 In this paper, the effects of different weight percentage of iridium (Ir) nanoparticles loadings on performance parameters of hydrazine catalyst and monopropellant thruster have been studied. Nanoparticles of iridium with different contents of 10 wt%, 20
Nooredin Ghadiri Massoom +5 more
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