机译:从地球表面开始使用混合动力推进小型火箭的效率分析
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk 630090;
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk 630090;
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk 630090;
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk 630090;
flight range; hypothetical small-size rocket; hybrid propulsion;
机译:混合动力火箭推进光学分析评估技术
机译:固体和混合火箭推进中氢化物的理论分析。
机译:在室内和室外特定表面上启动过程中手动轮椅推进的动力学分析
机译:荷载环形反应器概念分析荷敏火箭推进
机译:用火炬羽状模拟和温度测量的小型卫星混合火箭推进系统的开发
机译:采用渐进式混合检查的逐步应力部分加速寿命试验中掩盖式混合系统寿命数据的统计分析
机译:混合火箭推进系统光学分析评估技术