微型镓场发射电推力器的推力和比冲测量

电推进技术的发展推动了微推力测量技术和比冲测量技术的研究进程。为了评估已研制出的微型镓场发射电推力器的性能,进行了推力和比冲测量。研制了一种用于场发射电推力器的微推力测量平台;进行了LabVIEW开发;对测量平台进行了标定与分析,并通过试验比较了推力实测值与理论值,实测值范围为3~28μN。另外,利用飞行时间法,测得推力器在不同发射电流下的比冲数据,比冲范围为5917~8875s。     

红外及微波定标试验用空间环模设备研制

为了满足星载光学遥感仪器红外定标试验和星载微波遥感仪器微波真空定标试验的需求,上海卫星工程研究所研制成一套专用空间环模设备,该套设备在红外定标用20 K冷屏制冷方式的基础上,采用5台G-M制冷机组合冷却冷屏,冷屏温度可降至20 K以下。同时,该设备是国内第一台微波真空定标试验设备。试验证明设备各系统达到设计指标要求。     

支板喷射超声速燃烧火焰结构实验

为明晰支板喷射超声速燃烧火焰精细结构,并探索其影响因素,利用自发辐射成像技术和平面激光诱导荧光技术(PLIF)对支板喷射超声速燃烧流场进行研究。结果表明,燃烧室内形成了典型的扩散火焰,且火焰稳定在支板尾部的回流区,宽度与支板厚度处于同等量级;支板厚度和燃料喷注当量比对火焰结构有显著影响,增加支板厚度会使火焰基底变宽,火焰长度变短,有利于燃烧室内部的快速放热和缩短燃烧室长度,增加燃料喷注当量比会使火焰长度增加,燃烧强度增大。     

机体结构AE信号的统计分析研究

对机体结构声发射数据的表征参数进行分析,建立了数据处理的统计模型,并运用该模型分析了某型飞机全机疲劳试验和某现役飞机随机机载声发射监测数据,提出了结构损伤判据,可供实际应用。     

旋流预混预蒸发装置蒸发和排放特性

采用数值模拟和试验两种方法获得了两种结构的贫油预混预蒸发装置(Lean premixing and prevaporizing system,简称LPP)出口的油气混合均匀性,并采用单管燃烧室验证了LPP装置的燃烧特性.径向旋流预混装置出口的油气混合比轴向旋流预混装置更均匀;旋流器的叶片数和旋流角、预混管长度、气流速度、喷油方式等对油气混合均匀性均有比较显著的影响;在当量比高至0.5左右时,LPP燃烧室NOX和CO排放比传统燃烧室低得多;只要LPP装置出口存在回流,燃烧时就会出现回火现象.      

Magnetic connectivity and solar energetic proton event intensity profiles at deka-MeV energy

We present an analysis of the time-intensity profiles of 25 solar energetic proton events at 18.2 MeV, modelled by fitting an analytical function form (a modified Weibull function) to the observed intensities. Additionally relying on previous work that characterized the magnetic connectivity between the event-related solar flare and the observer in these events with three angular parameters, we investigate the fit function parameters, the connectivity parameters, and the iron-to-carbon ratio of the events for dependencies and correlations. We find that the fit parameter controlling the basic shape of the profile (parameter a) is not clearly dependent on the connectivity parameters or the Fe/C ratio, suggesting that the profile shapes of neither well and weakly connected nor generally “impulsive” and “gradual” events differ systematically during the early stages of the event at 1 AU. In contrast, the time scaling of the fit function (parameter b) is at least moderately correlated with both the magnetic connectivity parameters and the Fe/C ratio, in that well-connected and iron-rich events are typically shorter in relative duration than weakly connected and nominal-abundance events; intensity rise times display a similar correlation with the connectivity parameters. We interpret the former result as following from the combined effect of various transport processes acting on the particles in interplanetary space, while the latter is essentially consistent with established knowledge regarding the observed dependence of the time-intensity profile shapes of solar energetic particle events on their magnetic connectivity and heavy ion abundances. The desirability of modelling the particle transport effects in detail and extending the analysis to cover higher energies is indicated.     

Successes and challenges in non-destructive testing of aircraft composite structures

Composite materials are increasingly used in the aerospace industry. To fully realise the weight saving potential along with superior mechanical properties that composites offer in safety critical applications, reliable Non-Destructive Testing (NDT) methods are required to prevent catastrophic failures. This paper will review the state of the art in the field and point to highlight the success and challenges that different NDT methods are faced to evaluate the integrity of critical aerospace composites. The focus will be on advanced certificated NDT methods for damage detection and characterization in composite laminates for use in the aircraft primary and secondary structures.     

Reverberation time lags in the high luminosity quasar PG 1247+267

Virial estimates of the black hole mass in the center of AGNs, derived from single-epoch observations of luminosity and emission line widths, are now available for several thousands of objects at all redshifts and luminosities, so that studies of the cosmological evolution of the AGN mass function are becoming possible. These estimates are based on the empirical luminosity-size relation measured through reverberation mapping at low redshifts and luminosities. For this reason the spectrophotometric monitoring of 4 luminous quasars was started in 2003, with the 1.8 m telescope of the Asiago Observatory. To measure the reverberation time lag we adopt a method, recently introduced by Zu et al. (2011), which takes advantage of the available statistical information on variability autocorrelation and makes simple assumptions on the continuum-emission line transfer function. We present the estimate of the broad line region size for the quasar PG 1247+267, which is the most luminous object with reverberation measures to date. Virial products computed for C iv and C iii] emission lines provide consistent results. A possible flattening of the size-luminosity relation for C iv at high luminosity is suggested.     

复合固体推进剂损伤演化的声发射检测

导出了复合固体推进剂材料声发射(AE)累积能量与裂纹扩展间的线性关系,建立了基于声发射累积能量的损伤演化模型.单轴拉伸声发射实验结果验证了该演化模型的正确性,可用于复合固体推进剂材料损伤的研究.     

星载二次电源的电磁兼容预设计

针对星载二次电源电磁兼容试验中辐射发射的超标问题,提出了电磁兼容预设计方法.分析二次电源电磁干扰产生的机理,利用SPICE仿真器建立传导干扰的电路等效模型,优化电路设计得到传导干扰源;应用修正的单线模型近似计算辐射干扰,根据计算结果,利用遗传算法优化等效偶极子的数目和分布位置建立场等效模型;基于场路结合的方法,以传导干...