公开(公告)号：US20150107219A1

公开(公告)日：2015-04-23

申请号：US14403101

申请日：2013-05-07

申请人： Beijing Institute of Spacecraft Environment Engineering

发明人： Hua Zhao ,  Zhong Yi ,  Yuming Liu ,  Yenan Liu ,  Lifei Meng ,  Chao Zhang ,  Qi Xiao ,  Jipeng Sun ,  Yanlin Xu

IPC分类号： F03H1/00

CPC分类号： F03H1/0081 ,  F02K9/42 ,  F02K9/76 ,  F02K99/00 ,  F03H1/0012 ,  F03H1/0093

摘要： A chemical-electromagnetic hybrid propeller with variable specific impulse. Fuel gas ejected out from a spraying tube of the chemical propeller through chemical propulsion enters an ionization chamber through a first magnetic mirror tube for ionization. The fuel gas after ionization is heated up by radio-frequency ion cyclotron waves in an ion cyclotron wave heating chamber so as to improve the kinetic energy. Then a second magnetic mirror tube is used, so that ions in the fuel gas after the ionization are heated up many times in a reciprocating manner between the magnetic mirror tubes, and ejected to generate forward propulsion force. By means of the propeller, the propulsion force and the specific impulse are greatly increased.

摘要翻译： 具有可变比冲量的化学电磁混合推进器。 通过化学推进从化学螺旋桨的喷射管喷出的燃料气体通过用于电离的第一磁镜管进入电离室。 电离后的燃料气体通过离子回旋加热室中的射频离子回旋波加热，从而提高动能。 然后使用第二磁镜管，使得电离后的燃料气体中的离子在磁镜管之间以往复方式加热多次，并被喷射以产生向前推进力。 通过螺旋桨，推进力和比冲击大大增加。