Combustion of Silicon/Teflon/Viton and Aluminum/Teflon/Viton Energetic Composites [0.03%]
硅/特氟龙/维通与铝/特氟龙/维通含能复合材料的燃烧性能
Yarrington, Cole D.; Son, Steven F.; Foley et al.
Yarrington et al.
Thrust Stand Characterization of the NASA Evolutionary Xenon Thruster [0.03%]
美国国家航空航天局进化型氙离子推进器的推力台特性表征
Diamant, Kevin D.; Pollard, James E.; Crofton et al.
Diamant et al.
Engineering Model for Self-Pressurizing Saturated-N2O-Propellant Feed Systems [0.03%]
自增压饱和N₂O推进剂供给系统的工程模型
Whitmore, Stephen A.; Chandler, Spencer N.
Whitmore
Ion Propulsion Development Projects in U.S.: Space Electric Rocket Test I to Deep Space 1 [0.03%]
美国离子推进器研发项目：从空间电火箭试验I到深空1号
Sovey, James S.; Rawlin, Vincent K.; Patterson et al.
Sovey et al.
Powerplant Design and Performance Analysis of a Manned All-Electric Helicopter [0.03%]
载人全电动直升机的动力装置设计与性能分析
Datta, Anubhav; Johnson, Wayne
Datta
ROSFJORD, T. J.; ECKERLE, W. A.
ROSFJORD
Combustion characteristics of low flame temperature, chlorine-free composite solid propellants [0.03%]
低火焰温度、无氯复合固体推进剂的燃烧特性
KORTING, P. A. O. G.; ZEE, F. W. M.; MEULENBRUGGE et al.
KORTING et al.
DUTTON, J. C.
DUTTON
Johnston, W. A.
Johnston
Analysis of a Hybrid Dual-Combustion-Chamber Solid-Propellant Gas Generator [0.03%]
混合双燃烧室固体推进剂燃气发生器的分析
Freesmeier, Jon J.; Butler, P. Barry
Freesmeier