MEMS technology microthrusters and nanoenergetic materials for micropropulsion systems

K. Martirosyan, S. Lyshevski
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引用次数: 2

Abstract

Mini and micro air vehicles, missiles, guided munitions, projectiles and ordinances are controlled by control surfaces, thrust-vectoring and varying thrust. Microthrusters are key components of some classes of flight and naval vehicles. Solid-fuel rockets and microthrusters use solid propellants. Vehicles positioning, altitude control, orbital maneuver, aerodynamic orbit phasing and rotational manoeuvres are controlled. Enabled agility and maneuverability are achieved by advanced control schemes and propulsion systems. We examine microthrusters with solid propellants for micro- and miniature flight and naval vehicles. Fundamental, applied and experimental research and technology developments are performed by devising, designing and evaluating multi-physics MEMS technology microthrusters and propulsion systems with manoenergetic materials.
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微推进系统的MEMS技术微推力器和纳米能材料
小型和微型飞行器、导弹、制导弹药、射弹和军械由控制面、推力矢量和可变推力控制。微型推进器是某些级别的飞行器和海军飞行器的关键部件。固体燃料火箭和微型推进器使用固体推进剂。控制飞行器定位、高度控制、轨道机动、气动轨道相位和旋转机动。通过先进的控制方案和推进系统实现了灵活性和机动性。我们研究了用于微型和微型飞行和海军飞行器的固体推进剂微型推进器。基础、应用和实验研究和技术发展是通过设计、设计和评估多物理场MEMS技术微推进器和多能材料推进系统来完成的。
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