2001 Vol. 21, No. 3

Display Method:
ION-CYCLOTRON-RESONANCE HEATING MECHANISM OF THE HELY IONS IN LOWER SOLAR POLAR CORONA
SHU Chuanzheng, CHEN Fei, TU Chuanyi
2001, 21(3): 193-199. doi: 10.11728/cjss2001.03.20010301
Abstract:
In this paper, the four-fluid model, and replace O5+ with one of Fe11+, Mg9+, Mg7+, Ne7+, Si7+ ions respectively are adopted. The bulk velocity and temperature of the heavy ions are obtained, and compared with the SUMER observation data.
A THREE-DIMENSIONAL MHD SIMULATION FOR THE JANUARV 1997 SPACE WEATHER EVENT
SHI Yong, WEI Fengsi, FENG Xueshang
2001, 21(3): 200-207. doi: 10.11728/cjss2001.03.20010302
Abstract:
Based on observations from some satellites, observatories and the obtained definitely real solar wind backgroud, the propagation and evolution of the Janurary 1997 interplanetary CME were simulated in this paper using a 3-D MHD model. Results showed that the parameters simulated near the earth are in accordance with observations of WIND satellite, especially the temporal Bz behavior at 1 AU.
ALFVEN WWES IN THE MAGNETIC RECONNECTION REGIONS AND THE ACCELERATION OF NEWBORN IONS
WANG Xueyi, WU Jingsheng, LI Yi, WANG Shui, ZHAO Jikuen, CAO Jinbin
2001, 21(3): 208-218. doi: 10.11728/cjss2001.03.20010303
Abstract:
By means of 2D-hybrid simulation code, magnetic driven reconnection in the low plasma β case. Results show that the Alfven waves can be produced in the magnetic reconnection process. The newborn ions can be pitch angle scattered by Alfven waves and have the shell distribution. Some newborn ions are accelerated and the maximum energy is about 4miVA02/2. The acceleration takes about 100/Ωi and is thus extremely rapidly acceleration process.
ESCAPE OF MAGNETOSPERIC O+ OXYGEN IONS INTO THE MAGNETOSHEATH:MECHANISM AND EFFECTS
ZONG Qiugang, PU Zuyin, HUANG Zongying, FU Suiyan, B. Wilken
2001, 21(3): 219-229. doi: 10.11728/cjss2001.03.20010304
Abstract:
During the magnetic storm of January 10, 1997, Geotail spacecraft observed a mgnetospheric O+ burst event just on the outside of the dayside magnetopause. Energetic oxygen ions were seen to flow downward in the magnetosheath. The appearance of this O+ burst event was in close connection with the strong southward interplanetary magnetic field. The Principle Axis Analysis (PAA) indicates that the dayside magnetopause during this time period was a rotational discontinuity, magnetic reconnection took place in the magnetopause current sheet. Observations showed that reconnection was of the quasi-steady state type and that the O+ flow has a southward component. Both normal and inverse energy (velocity) dispersion were seen in the O+ flux enhancement process which were caused by the Time Of Fly (TOF) effect of oxygen ions escaping along the reconnected magnetic field lines. Only O+ can be transported by the gradient drift from the magnetosphere into the reconnection region, therefore they can be continuously detected in the magnetosheath. The escape rate of O+ in this event is estimated to be 0.61 × 1023 s-1, which was approximately 33% of the total input rate of the ring current oxygen ions. It is the escape of a great number of oxygen ions from the duskside of the inner magnetosphere (ring current region) that leads to the pronounced asymmetry in the ring current ASY-H index.
PARTICLE SIMULATION ON THE DYNAMICAL EVOLUTION OF RADIATION BELT PARTICLES
SHEN Chao, LIU Zhenxing
2001, 21(3): 230-237. doi: 10.11728/cjss2001.03.20010305
Abstract:
In this research, the spatial and temporal evolution properties of the external radiation belt particles during geomagnetic disturbances have been investigated by using a three dimensional relativistic electromagnetic particle code. The calculation shows that, the injected energetic protons and electrons perform bounce movements along geomagnetic field lines and can expand into the high latitude region. On the other hand, the injected protons and electrons also experience clockwise and anticlockwise magnetic drift movements, the larger the energy of the particles is, the faster the drift velocity will be. Multiple injections will cause a remarforble increase o f the flux of the external radiation belt particles.
LOW ALTITUDE SATELLITE ORBIT RADIAITION BELT PARTICLEENVIRONMENT VARIATION DUE TO GEOMAGNETIC LONG TERM VARIATION
LE Guiming, YE Zonghai, ZHOU Guocheng
2001, 21(3): 238-245. doi: 10.11728/cjss2001.03.20010306
Abstract:
Several typical low altitude orbits' radiation belt particle environment have been computed by using IGRF2000 and compared with those of using IGRF1970. The results show that the orbit integral flax's variation for protons with energy greater than 0.1 MeV reaches two order of magnitude for some inclination at the current part of the radiation belt. While the orbit integral flux for protons with energy greater than 10MeV reaches an order of magnitude for some inclination at same location of the radiation belt. The orbit's proton integral flux maximum variation is an order of magnitude. The electron integral flux's variation reaches up to three order of magnitude for some inclination orbit at lowest radiation belt radiation belt. The electron integral flux's maximum vaxiation is one of magnitude lower. The particle environment variation is little at the altitude greater than 1000 km.
THE CHARACTERISTIC OF TEMPERATURE AT HEIGHT OF 20-80km IN CHINESE AREA
MA Ruiping, XU Jiyao, LIAO Huaizhe
2001, 21(3): 246-252. doi: 10.11728/cjss2001.03.20010307
Abstract:
Some characteristics of temperature at height of 20-80km in Chinese area are obtained using the Nimbus-7 SAMS temperature data from 1979 to 1981 and are compared with of CIRA-1986. It is shown that the difference between the temperature above China with the zonal mean temperature of CIRA-1986 is obvious.
EFFECTS OF LEO'S ORBITAL ERRORS ON THE INVERSED MRAMETERS OF TERRESTRIAL ATMOSPHERE
JIANG Hu, HUANG Cheng
2001, 21(3): 253-258. doi: 10.11728/cjss2001.03.20010308
Abstract:
A numerical method is put forward to describe the effect of LEO's orbital errors on the inverted parameters of terrestrial atmosphere. Quantitative results are presented based on an occultation event on Oct.11, 1995. LEO's orbital errors show some features:temperature inversion precision at higher altitudes depends more on LEO's positional accuracy than that at lower altitudes in radial and transverse components, while it holds true the other other round in the normal component. Pressure inversion precision at higher altitudes depends less on LEO's positional accuracy than that at lower altitudes in normal and transverse components, while it holds true the other way round in the radial component. Inversion parameters at higher altitude are more insensitive to the velocity bias than that at lower altitude.
THE MEASUREMENT OF A SIMULATED OUTER SMCE PLASMA ENVIRONMENT IN GROUND LAB
PANG Yongjiang, XU Yuemin
2001, 21(3): 259-265. doi: 10.11728/cjss2001.03.20010309
Abstract:
The interaction between spacecraft and space plasma is important to the spacecraft's and its facilities' safety. But it is expensive and time-consuming to do experiments in outer space. In order to do such research in ground laboratory, a simulated space plasma environment is required to be set up. By using an ECR plasma resource and other facilities, an uniform plasma environment is obtained in a vacuum chamber.
STUDY OF METHODS FOR PREDICTING SEU RATE IN SPACE ORBITS
HE Chaohui
2001, 21(3): 266-273. doi: 10.11728/cjss2001.03.20010310
Abstract:
The methods for predicting Single Event Upset (SEU) rate abroad were analyzed. A method was proposed suitable for domestic status for predicting SEU rate. SEU rates and orbit specific rate coefficients were calculated in five typical orbits, and a tool is provided to assess the ability of semiconductor devices against SEU.
ORIGINAL NEPHOGRAM IF SIMULATOR FOR FY-2B SATELLITE
ZHANG Wei, PAN Zhangyong, YANG Zhixing
2001, 21(3): 274-279. doi: 10.11728/cjss2001.03.20010311
Abstract:
This paper introduced the original nephogram IF simulator for FY-2B Satellite. There are three parts in this device:burst data source, noise source and modulator. Theory and construction of each part is introduced in detail. This device has already been field tested and now using in the Command and Data Achieve Station of the satellite.
RESEARCH ON NUMERIC SIMULATION OF DOCKING DYNAMICS CONSIDERING INERTIA OF SHOCK ABSORBERS AND CONTACT DEFORMATION
GUAN Yingzi, CUI Naigang, KANG Weimin, ZHANG Chongfeng
2001, 21(3): 280-287. doi: 10.11728/cjss2001.03.20010312
Abstract:
Considering inertia of shock absorbers and contact deformation, a more precise and comprehensive docking dynamics model is built to make numeric simulation of the docking system which consists of two spacecrafts with androgynous peripheral docking mechanisms to reflect the dynamic characters of docking process. Types of contact points, geometrical model that determinates contact points, model of contact force and motion equations are studied. Simulation is done and the results are analyzed and compared with those which inertia and deformation are omitted.