In situ studies of electron density during equatorial spread-F

A Langmuir probe operated in fixed bias mode was launched onboard a RH-560 rocket from the Sriharikota Range (SHAR, Lat.13° 42'N, Geog. Long.80° 14'E, dip 10°) India on October 1, 1980 at 21h03 IST, to study the electron density profile and the electron density irregularities in the equatorial spread-F. The payload was designed to study medium and large scale irregularities. A highly variable and structured electron density profile was obtained. This was the first rocket launch in the Indian zone during spread-F condition.     

Structure of the equatorial lower ionosphere from the Thumba Langmuir probe experiments

A Langmuir probe designed and developed at the Physical Research Laboratory, Ahmedabad has been used on a variety of rockets since 1966 from the Thumba Equatorial Rocket Launching Station, TERLS (8°31'N, 76°52'E, dip.lat. 0°47'S) to study the structure of the equatorial lower ionosphere. Good quality data is available from a set of twenty five rocket flights conducted during the period 1966 to 1978. This data has been obtained using a single standardised instrument at a single location and using a uniform procedure for data reading and analysis, and adopting a calibration procedure to convert the measured probe currents into electron densities which involves a height dependent calibration factor. The data has been used to establish the gross features of the equatorial lower ionosphere under daytime, night time, morning twilight and evening twilight periods.     

Electric field and electron density measurements in the equatorial E-region

A centaure rocket, with payloads of Langmuir probe and Electric field probe, was launched from Thumba (8° 31'N, O° 47'S dip), India on February 12, 1981 at 1057 Hrs IST. The aim of the experiment was to study the role of localised electric fields in the generation of plasma density irregularities through cross field instability and the two-stream instability mechanism. The rocket was launched at a time when Type I irregularities were observed with VHF radar at Thumba.     

Proposals for an Indian standard tropical atmosphere up to 50 km

In an earlier report [1] the authors proposed an Indian Standard Tropical Atmosphere (ISTA1) from mean sea level to 20 km. This proposal describes adequately the mean conditions from 0° to about 30°N. The present work extends ISTA1 to the higher altitude of 50 km based oni. World Data Center A reports on Rocket firings [2],ii. M-100 rocket data for Thumba, India [3],iii. Northern Reference Atmospheres data of Cole and Kantor [4], andiv. Southern Reference Atmospheres data of Koshelkov [5].The proposed atmosphere, called ISTA7, has a sea level temperature of 30°C and a constant lapse rate of 6.5°C/km up to 16 km, as in ISTA1; from a temperature of -74°C at this altitude, there is a constant lapse rate of -2.3°C/km up to 46 km where the temperature is -5°C; the temperature remains constant thereafter up to 50 km. The fact that variations with longitude are weak except at very high latitudes [4], together with the fact that around 50 km, the temperature increases from low to high latitudes, lead us to propose a constant temperature of -5°C between 46 and 50 km, even though this temperature is slightly higher (by about 5°C) than the Thumba data.$\text{1}$/     

The POKER experiment: A 10,800 cm2 MWPC's array payload for hard X-Ray Astronomy

In this paper the POKER-HXR81M hard X-Ray payload is described. The instrument, designed and built at the Istituto di Astrofisica Spaziale of Frascati, is a very large array of MultiWire Proportional Counters (MWPC) devoted to stratospheric observations of cosmic sources in the field of hard X-Ray Astronomy. The payload basically consists of four passively collimated MWPC's having a geometric sensitive area of 2,700 cm² each with an efficiency higher than 10% in the operative range 15–200 KeV (80% at 60 KeV) with a square field of view of 5° × 5° FWHM. The overall spectral resolution is 13% at 60 KeV. The four MWPC's are filled with a very pure gas mixture of Xenon-Argon-Isobuthane at high pressure (3 bars).This experiment has been successfully flown during summer 1981 from the Milo balloon facility (Sicily, Italy). The performances of the payload and the preliminary results obtained during the 17 hours flight are discussed.     

A payload for the study of electric fields and electron density in the equatorial region

A rocket borne payload for simultaneous measurement of the electric field along and perpendicular to the rocket spin axis and the electron density in the medium was developed and flown from Thumba (8° 31′N, 0° 47′S dip) onboard two Centaure rockets for the study of plasma dynamcis in the equatorial E-region. The arrangement of sensors in this payload allows near continuous measurements of some of these parameters to be made.     

Measurements of upper atmosphere wind and temperature from meteorological rocket experiments during winter 1979

This institute conducted a series of meteorological rocket experiments for the upper-atmospheric sounding in the winter of 1979. Within the overlap altitude range with balloon flights, a comparison of the results with the standard radiosonde data indicated that the rocket-borne system was reliable. The measurements from foru rocket flights for the region between 20 and 30 km showed a degree of compatibility to each other while those for above 30 km differed considerably from one another. At low latitude, the temperature profiles in the winter stratosphere in general showed a reasonably good agreement with the U.S. Standard Atmospheric Supplements, 1966 (USSAS 66). A temperature of 2–24°C lower than the USSAS 66, however, was recorded in the lower mesosphere. Above 30 km the maximum diurnal variation in temperature was 9°C or so. In the winter, the wind profile showed the westerlies and the maximum wind velocity of 92.1 Msec^?1 was obtained from these experiments at the height of 60 km.     

鲲鹏elax-1B火箭头体分离后章动运动分析与仿真

2016年4月鲲鹏elax-1B探空火箭在海南儋州台站发射.箭头与箭体分离之后,瞬间进入大章动运动状态,超出预期设计的技术指标范围.基于这种运动现象,分析了鲲鹏elax-1B头体分离后箭头章动可能的产生原因,建立了稀薄大气下准刚体箭头的姿态动力学方程,并通过数字仿真方法模拟了箭头的章动运动.与实际飞行姿态进行对比,得出了导致章动发散的主要原因,为后续探空火箭的设计提供理论参考.      

The HESP/R satellite project

The aim of the HESP/R (High Energy Solar Physics/Radiation) satellite project is to obtain data of γ-ray, hard X-ray soft X-ray, EUV, and visible radiation of solar flares at the next solar maximum in order to study physics of flares. The HESP/R will be a spinning satellite of 4–5 rotations per min., and the spin axis is off-set by a small angle (0.5°–1.0°) from the Sun. Total weight will be 400 kg and launched in 1991 with M-3S-II rocket by ISAS.     

Energy deposition in the upper atmosphere in the EXCEDE III experiment

The EXCEDE III sounding rocket flight of April 27, 1990 used a 18 Ampere 2.5 keV electron beam to produce an artificial aurora in the region 90 to 115 km. A “daughter” sensor payload remotely monitored the low-energy X-ray spectrum while scanning photometers measured the spatial profile of prompt emissions of N₂⁺ (1N) and N₂ (2P) transitions (3914Å and 3805Å, respectively). Two Ebert-Fastie spectrometers measured the spectral region from 1800 to 8000Å. On the “mother” accelerator payload, the return current electron differential energy spectra were monitored by an electrostatic analyzer (up to 10 keV) and by a retarding potential analyzer (0 eV to 100 eV). We present an overview of the results from this experiment.     

冬季西北地区临近空间气象火箭探测数据分析

在获取冬季西北地区一次临近空间气象火箭探测数据后,将火箭探测温度、密度与MSIS00模式和TIMED/SABER卫星数据进行对比,并将火箭探测风场与HWM07模式和MERRA再分析资料进行对比,分析火箭探测温度误差组成,计算各项温度修正量。结果表明:火箭、卫星、MSIS00模式获取的温度和密度随高度整体变化趋势一致;相对于MSIS00模式,火箭和卫星实测数据能够反映出更多的变化细节,且二者在细节上具有较多一致性。火箭实测风场与MERRA的一致性较好,而与HWM07模式差异较大,在平流层中部火箭探测风场明显强于HWM07模式。相对于HWM07模式和MERRA,火箭探测风场能够体现更多细节,在22 km和45 km附近均探测到较强的风切变。在火箭探测温度的各项修正量中,气动加热、温度滞后、支撑结构热传导及测量电流焦耳效应带来的影响较大,该影响整体上随着高度降低而逐渐减小。分析表明,本次气象火箭获取的探测数据是有效可靠的,但在数据处理方法尤其是温度误差修正等方面还需不断迭代完善。      

Sea surface temperature measurement from satellites: Validation and accuracy

A review of the latest published results concerning the accuracy of satellite derived sea surface temperature (SST) estimation is presented. Two types of platforms are considered : orbiting satellites and geosynchronous satellites and the accuracies that may now be expected from such systems are reported. This review emphasizes the impressive improvement in global mapping of SST obtained from the Advanced Very High Resolution Radiometer (AVHRR) on NOAA's operational polar satellites. Tests of the AVHRR SST's against a high reliability data set consisting of buoys, bathythermographs and research ship reports indicate biases of < 0.1°C and RMS differences of < 0.75°C (McClain [1]). Particular attention is also paid to a method adding along track scanning capability to the present multichannel AVHRR technique. This method is demonstrated owing to the coupling of an orbiting satellite (TIROS-N) and a geosynchronous satellite (METEOSAT). Another type of coupling of two such platforms is also presented in connection with the advent of geostationary satellites equipped with a vertical sounding capability, such as GOES-4.     

瑞利激光雷达反演中层大气温度算法

瑞利激光雷达是探测中层大气温度的重要设备,具有高时空分辨率且不存在探测盲区的优点.为充分利用激光雷达探测到的原始数据,改进了传统的Chanin-Haunchecorne方法,采用由均匀搜索生成温度初值的方式反演大气温度.位于北京延庆（40.3°N,116.2°E）的瑞利激光雷达具有589nm和532nm两个通道,将589nm通道用于计算,532nm通道作为参考.在150~250K区间等间隔选取多个温度初值,利用589nm通道反演60~70km高度范围内的大气温度廓线和大气密度廓线,利用参考密度廓线选取准确的温度初值,反演得到准确的大气温度廓线.将589nm通道和532nm通道反演的温度廓线相比较,发现二者具有较高的一致性.改进后的方法有效利用了信噪比较差的光信号,使589nm通道的温度探测上限从60km提高到70km.      

Scientific results from the pioneer Saturn infrared radiometer

The Pioneer 11 Infrared Radiometer instrument made observations of Saturn and its rings in broadband channels centered at 20 and 45 μm and obtained whole-disk information on Titan. A planetary average effective temperature of 96.5±2.5 K implies a total emission 2.8 times the absorbed sunlight. Correlation with radio science results implies that the molar fraction of H₂ is 90±3% (assuming the rest is He). Temperatures at the 1 bar level are 137 to 140 K; regions appearing cooler may be overlain by a cloud acting as a 124 K blackbody surface. A minimum temperature averaging 87 K is reached near 0.06 bars. Ring boundaries and optical depths are consistent with those at optical wavelengths. Ring temperatures are 64–86 K on the south (illuminated) side, ～54 K on the north (unilluminated) side, and at least 67 K in Saturn's shadow. There is evidence for a south to north drop in ring temperatures. Titan's 45 μm brightness temperature is 75±5 K.     

Measurements of the energy spectra of charged particles within the vertical-10 rocket experiment

On December 21-st, 1981, at 18.35 hours UT from the territory of the USSR (coordinates - 49°N/L 2/) in implementation of scientific objectives and in accordance with the ‘INTERCOSMOS’ Programme, there was launched the heavy geophysical rocket ‘VERTICAL-10’. The scientific payload included a low-energy two-channel spectrometer for measuring the differential flows of electrons and protons within the energy range 0.1 to 10 keV, covered by 15 exponentially distributed energy levels.     

我国火箭探测资料与CIRA 1986稿的比较

本文用我国气象火箭探测获得的中层大气风、温度、密度和气压等数据,与国际参考大气模式CIRA 1986稿作了比较.结果看到,我国火箭探测温度数据值在模式给出的平均值剖面上下波动,符合的程度在国际比对偏差范围之内;用探测数据分析得到的风的季节性和声重波强度等与模式给出的描述都很符合.从而说明,用CIRA 1986稿来表征我国上空的中层大气结构是合适的.      

Measurements of electrical breakdown in the vicinity of a sounding rocket differentially charged to 10 kV

During the initial period of high voltage biasing of the SPEAR-3 sounding rocket payload, it was observed that electrical breakdown occurred in the gas surrounding the rocket. The breakdown occurred almost all the way to apogee of 289 km on the upleg, but did not recur on the downleg until the payload reached an altitude of 100 km. It is suggested that this behavior can be attributed to payload outgassing on the upleg leading to abnormally high gas pressure near the payload skin. Consideration of a modified Paschen discharge process with varying pressure along the discharge path was found to be consistent with the results.     

Registration of ELF waves in rocket-satellite experiment with plasma injection

Two rocket experiments KOMBI-SAMA with plasma injection at height 100–240 km were performed in August 1987 in the region of Brazilian magnetic anomaly (L = 1.25). The launching time of the rocket was determined so that plasma injection was at the time when satellite COSMOS 1809 passed as close as possible to magnetic tube of injection. Caesium plasma jet was produced during ≥ 300 s by electric plasma generator separated from the payload. By diagnostic instruments on board of the rocket and the satellite were registered energetic particle fluxes and plasma wave activities stimulated by plasma injection. When the satellite passed the geomagnetic tube intersecting the injection region an enhancement of ELF emission at 140 Hz, 450 Hz by 2 times was registered on board the satellite. An enhancement of energetic particles (E > 40 keV) flux by 4–5 times was registered on board the rocket. Observed ELV emission below 100 Hz is interpreted as generation of oblique electromagnetic ion-cyclotron waves due to drift plasma instability at the front of the plasma jet.     

Long duration hard X-ray transatlantic payload

This note describes the HXR80M large area hard X-Ray Astronomy experiment. The payload is scheduled for a flight on board of a transatlantic balloon to be launched the next July from the Milo Base (Sicily), in the framework of the CNR experimental transatlantic campaign.The detectors are two Multiwire Spectroscopic Proportional Chambers (MWSPC) having 2,700 cm² sensitive area each.The two detectors are filled with an extremely pure Xenon-Isobutane mixture (impurity less than 1ppm) at high pressure (3–6 Atm) in order to obtain good spectral resolution and high efficiency. The field of view of the MWSPC's is limited by an array of three collimators each, having respectively 8°×8° and 5°×5° FWHM.The on board data handling is performed by microprocessor controlled electronics. In particular a micro Multichannel Analyzer (μMCA) is employed to obtain the spectrum of the detected photons. The scientific and housekeeping data are send to ground through a 1.2 Kbit PCM HF Telemetry link.The scientific aim of the experiment is the survey of the sky belt around the 38th parallel and in particular the observation of faint galactic objects and galactic binary systems in the range 15–200 keV.     

Ultraviolet spectroscopy of the chromosphere and transition zone at high spatial and temporal resolution

The third rocket flight of the NRL High Resolution Telescope and Spectrograph (HRTS) recorded UV spectra of the quiet Sun in a 10″ × 800″ region. By rastering the slit in 2′' increments, a time series with 20s resolution of two-dimensional spectra with 1′' spatial resolution was obtained. The spectrum includes strong chromospheric diagnostic lines of C I, Si I, and Fe II, transition zone lines of C IV and the continuum which is produced in the temperature minimum. Images of the network show that Fe II emission is well-correlated with dark Hα mottles, that the transition zone is produced in extended structures which are apparently continuations of the mottles, and that the strongest continuum emission is from near the base of the mottles. Time series of C I profiles show little variation in most features aside from the chromospheric jets which develop rapidly over timescales of 30s. The C IV profiles also show only gradual variations over most of the slit except for the numerous small explosive events.