大气臭氧与气溶胶垂直分布的高空气球探测

本文给出了1993年9月12日利用高空科学气球在河北省香河地区探测到的大气臭氧和气溶胶的垂直分布。结果发现:(1) 大气臭氧的数密度在整个对流层较低(～10[12]mol/cm3)，并从地面到对流层顶略有下降；对流层顶以上开始快速增加，极值层高度在～24 km，其值为4.78×10[12]mol/cm3；臭氧分压有类似的分布特征，极值146×10[-4]Pa，位于同一高度；(2) 在平流层低层，臭氧分压有一个次极值62×10[-4]Pa，位于15～16 km；(3) 0～30 km大气气溶胶数密度呈现出三个峰值:143，8和1.1 个/cm[3]，分别位于近地面、5 km和21 km；（4）气溶胶的数密度谱在对流层为双模态；在平流层，次峰消失。同时，我们还与其他观测结果作了比较分析。     

The thermodynamic structure atop a penetrating convective thunderstorm

The thermodynamic structure on top of a numerically simulated severe storm is examined to explain the satellite observed plume formation above thunderstorm anvils. The same mechanism also explains the formation of jumping cirrus observed by Fujita on board of a research aircraft. A three-dimensional, non-hydrostatic cloud model is used to perform numerical simulation of a supercell that occurred in Montana in 1981. Analysis of the model results shows that both the plume and the jumping cirrus phenomena are produced by the high instability and breaking of the gravity waves excited by the strong convection inside the storm. These mechanisms dramatically enhance the turbulent diffusion process and cause some moisture to detach from the storm cloud and jump into the stratosphere. The thermodynamic structure in terms of the potential temperature isotherms above the simulated thunderstorm is examined to reveal the instability and wave breaking structure. The plumes and jumping cirrus phenomena represent an irreversible transport mechanism of materials from the troposphere to the stratosphere that may have global climatic implications.     

Radiance and color of the sky at twilight: Perturbations caused by stratospheric haze

Layers of stratospheric aerosol with optical thicknesses as small as 10^–4 cause noticeable perturbations in the monochromatic logarithmic brightness gradient,G, and the color ratio,C, of the twilight sky. Modeling of the twilight's radiant properties shows that definite single-valued relationships exist between maxima inC or minima inG and optical thickness, , physical thickness h, and mean altitude, , of stratospheric layers. It is therefore possible to determine , h and and monitor their variations by performing either single wavelength measurements ofG or two-wavelength spectrophotometric measurements ofC. The presence of haze in the lower troposphere and the occurrence of multiple scattering both have relatively minor influences on the recovery of the stratospheric dust properties, provided that 10< <30 km.Formal mathematical inversions of the single-scattering twilight equations are possible in principle, but difficult in practice because of non-linearities. Inversions incorporating an iterative linearization process with constrained smoothing, successfully recovered the features of the haze layer, but tended to oversmooth the vertical profile and underestimate the mean altitude of the haze layer.     

Structure and dynamics of the stratosphere and mesosphere revealed by VHF radar investigations

Powerful VHF radars are capable of almost continuously monitoring the threedimensional velocity vector and the distribution of turbulence in the middle atmosphere, i.e. the stratosphere and mesosphere. Methods of radar investigations of the middle atmosphere are outlined and the basic parameters, mean and fluctuating velocities as well as reflectivity and persistency of atmospheric structures, are defined. Results of radar investigations are described which show that the tropopause level as well as a criterion on the stability of the lower stratosphere can be deduced. Besides mean wind velocities, VHF radars can measure instantaneous velocities due to acoustic gravity waves. The interaction of gravity waves with the background wind is discussed, and it is shown that cumulus convection is an effective source of gravity waves in the lower stratosphere. The vertical microstructure of the stratosphere, manifesting itself in thin stratified sheets in which temperature steps occur, is investigated by applying knowledge from investigations of the oceanic thermocline. Possible origins, like shear generation and lateral convection of the microstructure of the stratosphere, are discussed. Observations of gravity waves in the mesosphere are reviewed and their connection with turbulence structures is pointed out. Finally, some open questions which could be answered by further VHF radar investigations are summarized.     

Measurement of lower-stratospheric aerosol by a balloon-borne photometer

Height distribution of the stratospheric aerosol extinction coefficient was measured in the altitude range 10 to 20 km by a balloon-borne multi-color sunphotometer in May 1978. It is demonstrated that detailed structures of the distribution of stratospheric aerosol can be remotely measured by the solar occultation method as well as by lidar andin situ particle counter observations. In the aerosol layer appearing at 18 km altitude the extinction coefficient at 800–1000 nm wavelength reached to 3×10^–7 m^–1, which was reasonable compared with lidar observations. Wavelength dependence of the aerosol optical depth was crudely estimated to be proportional to ^–1.5.     

Upper Limit of Iodine Oxide in the Lower Stratosphere

It has been suggested that iodine oxides, IOx, could play a significant role in the ozone destruction in the lower stratosphere. To investigate this suggestion, spectra from nine SAOZ uv-visible spectrometer balloon flights were examined for the IO absorption signature between 405 and 450 nm. IO was not detected, either at mid- or high latitude, in the morning or the evening, in summer or winter. An upper limit of 0.2 parts per trillion by volume (pptv) at 20 km and 0.1 pptv at 15 km at the 95% confidence level (2), was derived from the best measurements at 90° SZA at sunset and sunrise. Since a photochemical model shows that 70% of inorganic iodine should be in the form IO at that time, it is concluded that unless iodine chemistry is different from that assumed at the moment, the role of iodine in stratospheric ozone depletion is small.     

高空探测资料气球空间经纬度偏差算法

随着数值预报的发展,模式的分辨率逐渐提高,探空气球在施放过程中受高空气流影响造成的漂移已大大超出了数值预报模式分辨率,其影响不能忽视。鉴于现有气球空间位置经纬度偏差计算方法基于站心坐标系,忽略地球曲率影响,文章从探测系统原理出发,推导出精确的基于地心坐标系的气球空间位置经纬度偏差计算公式,并通过探空数据文件对原有算法进行误差分析。     

2007/2008和2008/2009冬季平流层强、弱极涡事件对应的行星波活动的对比分析

在对逐日气象资料进行纬向谐波分析的基础上, 对比和讨论了2007/2008年冬季强极涡期间和2008/2009冬季弱极涡期间平流层和对流层不同波数的行星波的变化特征, 特别关注强极涡或弱极涡发生之后, 500 hPa 沿60°N和30°N行星波1波和2波振幅和位相的差异, 以及相应的500 hPa位势场的差异, 进而讨论为什么不同的平流层极涡异常会对东亚有不同的影响, 特别讨论为什么同一种极涡异常, 对我国南北方近地面气温的影响会不同。结果表明:平流层极涡发生异常时, 平流层行星波活动有明显的异常。随着极涡异常的下传, 对流层行星波的振幅和位相也有明显的变化, 而且, 对于不同的纬度带, 其变化又有不同, 表现为:2008年1月强极涡发生之后, 500 hPa行星波1波和2波的扰动都向南伸, 而2009年1月的弱极涡(SSW)期间和之后, 1波和2波的扰动都偏北; 在对流层, 强极涡和弱极涡发生之后不但行星波1波和2波的振幅有所差异, 其位相也有明显的不同。特别是, 其位相的差异还随纬度而变化。就同一年(或者说对于同是强极涡或者同是弱极涡)而言, 无论是1波还是2波, 在60°N和30°N附近的扰动相比, 几乎反位相。这样就使得它们的500 hPa 位势场也有明显不同:在东半球, 主要表现为乌拉尔高压和东亚大槽的强度和位置不同。2008年1月强极涡发生之后, 乌拉尔高压和东亚大槽东移, 不利于冷空气向欧亚大陆北部(包括我国北方)的输送, 使这些地区的温度偏高;而2009年1月弱极涡之后, 东亚大槽西退, 利于冷空气向欧亚大陆北部输送, 导致这些地区较冷。对于同一种极涡异常(如2008强极涡或者2009弱极涡)由于南方和北方行星波扰动的位相不同, 对南方和北方冷暖空气的输送也就不一样。所以同一种极涡异常对(我国)南北地区的温度影响是不同的。     

未来甲烷排放增加对平流层水汽和全球臭氧的影响

利用一个耦合的大气化学-气候模式(WACCM3)研究了地表甲烷排放增加对平流层水汽和全球臭氧变化的影响.结果表明,如果地表甲烷的排放量在2000年的基础上增加50%(达到政府间气候变化专门委员会A1B排放情景中2050年的值),平流层水汽体积分数将平均增加约0.8×10^-6.南半球平流层甲烷转化为水汽的效率比北半球高.在北半球平流层中,1mol甲烷分子可以转化为约1.63mol的水汽分子,而在南半球1mol甲烷分子大概可以转化为约1.82mol的水汽分子.甲烷排放增加50%将使全球中低纬度地区以及北半球高纬度地区的臭氧柱总量增加1%-3%,使南半球高纬度地区臭氧柱总量增加近8%,而秋季(南半球春季)南极地区臭氧柱总量增加幅度可高达20%,南极臭氧的这种显着增加主要是由于甲烷增加造成的化学反馈所致.在北半球中高纬度地区,甲烷增加引起的臭氧变化主要与甲烷氧化导致的水汽增加有关.研究还表明,未来甲烷排放增加对臭氧的恢复作用其实与溴化物排放的减少一样重要.     

InFOCμS Hard X-ray Imaging Telescope

InFOCμS is a new generation balloon-borne hard X-ray telescope with focusing optics and spectroscopy. We had a successful 22.5-hour flight from Fort Sumner, NM on September 16,17, 2004. In this paper, we present the performance of the hard X-ray telescope, which consists of a depth-graded platinum/carbon multilayer mirror and a CdZnTe detector. The telescope has an effective area of 49 cm² at 30 keV, an angular resolution of 2.4 arcmin (HPD), and a field of view of 11 arcmin (FWHM) depending on energies. The CdZnTe detector is configured with a 12 × 12 segmented array of detector pixels. The pixels are 2 mm square, and are placed on 2.1 mm centers. An averaged energy resolution is 4.4 keV at 60 keV and its standard deviation is 0.36 keV over 128 pixels. The detector is surrounded by a 3-cm thick CsI anti coincidence shield to reduce background from particles and photons not incident along the mirror focal direction. The inflight background is 2.9 × 10⁻⁴ cts cm⁻² sec⁻¹ keV⁻¹ in the 20–50 keV band.