...
机译:液态氢对火箭推进剂加载的动力学模型
MCT, Inc., Moffett Field, California 94035,Federal Contractor, NASA Ames Research Center,Applied Physics Group, Moffett Field, CA 94035;
University of California, Santa Cruz, Moffett Field, California 94035,Federal Contractor,NASA Ames Research Center, Applied Physics Group, Moffett Field, CA94035;
New Jersey Institute of Technology, Newark, New Jersey 07102,NASA Ames Research Center, Department of Mathematical Sciences, Moffett Field, CA 94035;
SGT, Inc., Newark, New Jersey 07102,Federal Contractor, NASA Ames Research Center,Applied Physics Group, Moffett Field, CA, 94035;
NASA Ames Research Center, Moffett Field, California 94035,Federal Contractor, NASA Ames Research Center, Applied Physics Group, Moffett Field, CA 94035;
NASA Marshall Space Flight Center, Huntsville, Alabama 35805;
A: cross-sectional area of storage tank, pipe, or liquid/vapor interface in storage tank, m~2; c_(p(V)): constant pressure (volume) specific heat, J/K • kg; d_r: wall roughness, m; f: dimensionless resistance coefficient; H: height of external tank, m et al;
机译:在氢和氧作用下的液体火箭发动机中碳-碳复合材料制成的模型喷嘴延伸量的长期测试
机译:在氢气和氧气上运行的液体推进式火箭发动机中由碳 - 碳复合材料制成的模型喷嘴延伸的长期测试
机译:含推进剂的柔性液体火箭的多体动力学
机译:溶解氦气压力对液体氢火箭推进剂罐的影响建模
机译:比例对氢/氧液体推进剂火箭发动机排气性能的影响。
机译:液体火箭推进剂工作人员的肝脏检查
机译:核火箭系统辐射屏蔽设计与分析的综合。体积I.使用模拟液体氢气的核火箭推进剂罐模型中的辐射测量
机译:核火箭系统辐射防护设计与分析计算方法的综合。第1卷 - 使用模拟液态氢的核火箭推进剂罐模型中的辐射测量