National Key Laboratory of Combustion, Flow and Thermo-Structure, Northwestern Polytechnical University, Xi’an 710072,China;
National Key Laboratory of Combustion, Flow and Thermo-Structure, Northwestern Polytechnical University, Xi’an 710072,China;
School of Aeronautics and Astronautics, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, Liaoning, China;
National Key Laboratory of Combustion, Flow and Thermo-Structure, Northwestern Polytechnical University, Xi’an 710072,China;
National Key Laboratory of Combustion, Flow and Thermo-Structure, Northwestern Polytechnical University, Xi’an 710072,China;
solid propellant; MEMS-based solid propellant micro-thruster; lead styphnate; thermal decomposition; ignition;
机译:微型推进器用固体推进剂的燃烧行为
机译:使用实际推进剂燃烧率的实际依赖性对压力的实际依赖性计算固体推进剂火箭电动机的压力
机译:基于MEMS的固体推进剂微分器(SPM)阵列的优异性能与纳米液体
机译:基于MEMS的固体推进剂微推进器的固体推进剂研究
机译:研究含能多孔硅作为固体推进剂微推进器
机译:在所有固态高氯酸盐ISE中作为固体接触的单壁碳纳米管(SWCNT):在烟花爆竹分析中的应用
机译:用于太空和军事应用的基于mEms的固体推进剂微型推进器阵列
机译:使用微探针质谱仪(mpms)系统研究固体推进剂的气相化学:固体燃料(HTpB / Zecorez和BamO / NmmO),单基推进剂(m10)和RDX基推进剂(BLX-)的初步结果9)。