Aerosol concentrations and size distribution in the troposphere and lower stratosphere over Thumba

Rocket-borne ultraviolet photometers operating at =0.31 m have been used at Thumba (8°33N, 76°52E) to make measurements of atmospheric scattering at tropospheric and lower stratospheric altitudes. Measurements could be made of the amplitude of the scattered fluxes and the angular distribution up to an altitude of about 24 km on three rocket flights conducted as part of the 16 February 1980 solar eclipse campaign. These measurements have been used to study the size distribution as well as the number densities of aerosols in the troposphere and lower stratosphere over Thumba.     

利用光变曲线估计猎鹰九号火箭末级的旋转状态研究

光度观测是地基观测空间目标的主要手段之一,利用光度信息能够估计空间目标的相关特征信息。为了更好地了解空间目标的旋转状态,选取具有代表性的猎鹰九号火箭末级作为研究对象,由其光变信息研究旋转状态。首先利用云南天文台1.2 m光学望远镜获取猎鹰九号火箭末级的光度数据,再对目标星等进行斜距归一化,得到目标光变信息并分析目标星等随时间变化的曲线,估计大致的旋转周期,再由相位离散最小化方法计算会合周期。根据太阳、目标和测站之间的位置关系、惯性主轴指向、旋转轴指向、初始相位等因素,采用姿态旋转矩阵计算理论星等,利用最小二乘原则确定惯性主轴方向及初相角度、旋转轴指向。最后给出了猎鹰九号火箭末级的旋转周期、会合周期以及旋转轴指向等参数,为后续开展其他空间目标光度信息研究提供参考。     

利用多普勒天气雷达估算对流云火箭增雨防雹用弹量的方案

利用新一代多普勒天气雷达产品资料,结合人工影响天气原理,引用人工影响天气数值实验的人工冰核浓度等有关参数,将垂直累积液态含水量(VIL)及回波顶高度(ET)等导出产品合理地应用于火箭增雨防雹作业用弹量计算公式中,解决了以前人为或间接估计对流云作业区体积及其含水量的难题,提出客观定量计算人工增雨防雹作业用弹量的初步方案,并以其计算的用弹量为主要参数设计火箭作业参数指挥界面.经2005年一次增雨作业应用检验,证明结果切实可行,对节约人工影响天气成本,有效指导对流云火箭增雨防雹作业具有一定的意义.     

Disturbances of the ionosphere of blast and acoustic waves generated at ionospheric heights by rockets

In this paper we present a model, which describes the propagation of acoustic impulses produced by flight of rockets through a model terrestrial atmosphere, and effect of these impulses onto the ionosphere above a rocket. We show, that experimentally observed ionospheric disturbances with duration about 300 s cannot be explained by effect of acoustic impulses onto the ionosphere. We have calculated parameters of a blast wave produced by launch vehicle on the ionospheric heights. It was shown that the blast wave is intense and this wave can generate great disturbance of electron density. The disturbance of electron density can exceed the ambient electron density in 2.6 times. We supposed that the observed ionospheric disturbances might be produced by propagation of delayed magnetoacoustic wave, which, in turn, was produced by the blast wave.     

江西省BL-1型火箭增雨作业技术方法研究

在对BL-1型增雨火箭特性进行分析的基础上。结合江西全年增雨作业的特点，对BL-1型火箭的人工增雨作业技术进行了分析研究。旨在提高一线火箭作业人员的业务技术，进而提高人工增雨作业的成功率和降水效率。     

微火箭电场仪的原理及其应用

介绍一种新型的雷雨云电场探测仪器---微火箭电场仪 ,由直径为 55mm×760mm农用消雹小火箭改装而成 .它利用导体在电场中感应电荷原理 ,由电场传感器、测量线路、1 680MHz遥测发射机及天线组成 .仪器特点是结构简单、高密集、超小型、快速机动、低功耗、低成本 .此仪器于 1 998年年初试飞成功 .电场探测范围 1- 1 0 0kV/m .探测高度为7 5km左右 .主要用于飞行器升空安全保障 ,以及气象部门对雷电、冰雹的探测和预警     

Rocket observations of atomic oxygen density and airglow emission rate in the WAVE2000 campaign

Atomic oxygen density and airglow volume emission rate profiles measured in the rocket experiment S-310-29 carried out as a part of the Waves in Airglow Structures Experiment over Kagoshima in 2000 (WAVE2000) campaign are presented, and the excitation processes of the atomic oxygen 557.7 nm line and the molecular oxygen atmospheric band airglow emissions are discussed. The volume emission rate profiles calculated from the measured atomic oxygen densities using the methods and parameters proposed by the ETON campaign (EATON model) are found to well represent the shapes of measured twin-peak emission rate profiles seen during this campaign suggesting that the EATON model is valid for a perturbed atmosphere. There is some discrepancy in the modeled absolute values for the emissions. Applying the model to the current O density measurements results in predicted emission rates that are a factor of 3.2 and 1.5 too high for the 557.7 nm line and Atmospheric band, respectively. This suggests either that the atomic oxygen densities of the present campaign are too large by a factor of 1.2 (=1.5^1/2) to 1.5 (=3.2^1/3), or that those of the ETON campaign were too small by the same factor or that the combined errors in both campaigns can account for the discrepancy (the modeled volume emission rates of the 557.7 nm line and atmospheric band are roughly in proportion to [O]³ and [O]², respectively). Our present data findings do not favor the 2-step more than the 1-step excitation process for the atmospheric band because a calculation of the quantum efficiency based on the observed O density does not show a steep gradient around 100 km.     

夏季对流云火箭增雨技术初步研究

该文着重讨论了利用具有射程远，播撒高度高，催化剂量大，成核率高等优点的增雨火箭，对对流云进行催化时目标云的选择、催化潜力判断、催化时机把握、催化部位的确定以及运用雷达来指挥作业等关键问题进行了研究。分析了当地地形气候特点、对流云雷达回波特征、作业工具特点等资料，并通过模式对催化剂量（火箭用弹量）进行模拟计算，以及充分考虑现有的人工影响天气技术水平、装备设施和通讯条件等，提出了包括客观作业指标、监测预警流程、作业参数生成、指挥通讯方式和效果观测收集等内容的火箭增雨作业技术方法。     

Slow Z-mode radiation from sounder-accelerated electrons

Quasi-electrostatic Z-mode waves created by the transmitting part of the OEDIPUS-C payload were measured on the receiving part at 1200 m distance. Solutions of the complete electromagnetic dispersion relation for a hot magnetoplasma reveal, however, that there is no solution that provides direct ray paths along the transmitter-receiver separation direction with the observed signal group delays. An interpretive model is therefore proposed in which sounder-accelerated electrons (SAE) radiate incoherently as they spiral along the magnetic field direction in the general direction of the receiving subpayload. Test-particle theory combined with the hot-plasma dispersion solution is used to predict the total electric field for previously reported SAE flux levels. It is found that voltage levels measured on the receiving dipoles have about the same order of magnitude as the predicted ones.     

用改进的SPEA求解轨道转移的时间-能量极小化问题

提出了改进的SPEA，这是一种多目标进化算法，适于求解大尺度空间的多目标优化的Pareto最优解，并应用于求解轨道转移的时间—能量极小化问题，计算结果表明算法的有效性。