The efficacy of spacecraft propulsion systems significantly depends on the choice of propellant.This study utilized laser-induced breakdown spectroscopy(LIBS)to investigate the impact of different fuel types,fuel rati...
co-supported by NSAF,China(No.U1730134);the National Natural Science Foundation of China(No.11772310);the Innovation Foundation for Doctor Dissertation of Northwestern Polytechnical University,China(No.CX202034);the Innovation and Entrepreneurship Fund of the Student Affairs Department of Northwestern Polytechnical University,China(No.2021-CXCY-005)。
As a novel micro-propulsion system for small satellites(from micro to nano),the ionic liquid electro spray propulsion system is a promising candidate.However,performance measurement and evaluation of the Ionic Liquid ...
supported by National Natural Science Foundation of China (Nos. 11502301, 11602304 and 62175260)
In order to optimize the laser ablation performance of a micro-thruster with 1U dimensions,which employs a micro semiconductor laser,the impacts of pulse width and glycidyl azide polymer(GAP)thickness on thrust perfor...
The International Conferences on Micropropulsion and Cube Sats focus on science,design,and application of micropropulsion platforms,systems and devices for small satellites and Cube Sats,as well as miniaturized propul...