Microelectromechanical propulsion systems for spacecraft

摘要: Abstract : This is a survey of current research on micropropulsion options for very small satellites (less than ten kilogram). The concentration and performance evaluations utilize Micro Systems Technology (MST) Electromechanical technology (MEMS) integrated with existing theories. State the art methods used design manufacturing MEMS devices are included to provide size perspective microthruster technology. Nine viable presented, including detailed analysis pulsed Plasma Thruster. Exploration future role in space influential factor benefiting efforts extremely scale microthrusters. significant background information astrodynamics assist intended reader: student Engineering Science interest Aerospace Propulsion Industry.