Results 171 to 180 of about 32,742 (216)
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Microcooling Channel Effect on a Monopropellant Microelectromechanical System Thruster Performance
Journal of Propulsion and Power, 2017AS MICROELECTROMECHANICAL system fabrication technology advances, the aerospace industry, in pursuing smaller, faster, and cheaper satellites, sees several opportunities for effective satellite operations. Miniature satellites with 1–10 and 10–100 kg masses are called nanosatellites and microsatellites, respectively; and they offer the advantages of ...
Huh, J, Kwon, S
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Journal of Propulsion and Power, 2018
Hydroxylammonium-nitrate-based monopropellant thrusters have been continuously researched as a replacement for conventional hydrazine thrusters.
Asato Wada +2 more
semanticscholar +1 more source
Hydroxylammonium-nitrate-based monopropellant thrusters have been continuously researched as a replacement for conventional hydrazine thrusters.
Asato Wada +2 more
semanticscholar +1 more source
Endurance Tests on Different Catalytic Beds for H2O2 Monopropellant Thrusters
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2009The present paper illustrates a comprehensive experimental campaign carried out in order to assess the capability of four especially-developed catalytic beds to decompose hydrogen peroxide under operational conditions representative of typical application to small monopropellant rocket engines, and to characterize the resulting performance of the ...
PASINI, ANGELO +4 more
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Design, fabrication and thrust measurement of a micro liquid monopropellant thruster
Journal of Micromechanics and Microengineering, 2014A liquid monopropellant MEMS thruster was designed, fabricated and tested. For application on a nanosatellite for orbit control, a liquid propellant MEMS thruster delivers better performance than a solid thruster. Two issues must be addressed for a liquid monopropellant MEMS thruster: high energy content of the monopropellant to overcome the excessive ...
Huh, JM Huh, Jeongmoo +1 more
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Test Bench for the Unsteady Characterization of a Pulsed Green Monopropellant Thruster
51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015PulCheR is a R&D project funded by the European Union Seventh Framework Programme with the main aim of demonstrating the feasibility of a new propulsion concept in which the propellants are fed in the combustion chamber at low pressure and the thrust is generated by means of high frequency pulses.
PACE, GIOVANNI +2 more
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EXPERIMENTAL ASSESSMENT OF HYDROGEN PEROXIDE DECOMPOSITION IN A MONOPROPELLANT THRUSTER
International Journal of Energetic Materials and Chemical Propulsion, 2011BONIFACIO, SALVATORE +2 more
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Preliminary design and study of 5N HTP monopropellant thruster for small satellites
Acta Astronautica, 2023Giuseppe Gallo +2 more
exaly
Design and experimental research of a sub-Newton N2O monopropellant thruster with inner-heater
Chinese Journal of Aeronautics, 2022Kaiyang Li, Jie Fang, Guobiao Cai
exaly
N2O Decomposition on Ru/Si-doped Alumina Catalyst for Monopropellant Thruster
Journal of Propulsion and EnergyMyoungjin Kim, Taegyu Kim
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