排序方式: 共有38条查询结果,搜索用时 15 毫秒
21.
A.N. Parmar J.L. Culhane C.G. Rapley K.J.H. Phillips C.J. Wolfson L.W. Acton B.R. Dennis 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1982,2(11):151-154
The Bent Crystal Spectrometer on the NASA Solar Maximum Mission satellite provides high spectral and temporal resolution observations of the Fe Kα lines. We have analysed spectra from almost 50 solar flares that occurred during 1980. These data strongly support fluorescent excitation of photospheric iron by photons of E > 7.11 keV emitted by the hot coronal plasma produced during the flare. After comparison of the data with a model, we discuss the observed Kα line widths, estimates of the size of the emitting region, the height of the coronal source and the photospheric iron abundance. 相似文献
22.
J. T. Gosling S. J. Bame D. J. Mccomas J. L. Phillips A. Balogh K. T. Strong 《Space Science Reviews》1995,72(1-2):133-136
Nine coronal mass ejections (CMEs) have been detected in the solar wind by the Ulysses plasma experiment between 31° and 61° South. One of these events, which was also a magnetic cloud, was directly associated with an event observed by the soft X-ray telescope on Yohkoh in which large magnetic loops formed in the solar corona directly beneath Ulysses. This association suggests that the flux rope topology of the magnetic cloud resulted from reconnection between the legs of neighboring magnetic loops within the rising CME. The average CME speed (740 km s–1) at these latitudes was comparable to that of the normal solar wind there and is much greater than average CME speeds observed either in the solar wind in the ecliptic plane or in the corona close to the Sun. We suggest that the same basic acceleration process applies to both slow CMEs and the normal solar wind at any latitude. 相似文献
23.
Suess S. T. Phillips J. L. McComas D. J. Goldstein B. E. Neugebauer M. Nerney S. 《Space Science Reviews》1998,83(1-2):75-86
The solar wind in the inner heliosphere, inside ~ 5 AU, has been almost fully characterized by the addition of the high heliographic latitude Ulysses mission to the many low latitude inner heliosphere missions that preceded it. The two major omissions are the high latitude solar wind at solar maximum, which will be measured during the second Ulysses polar passages, and the solar wind near the Sun, which could be analyzed by a Solar Probe mission. Here, existing knowledge of the global solar wind in the inner heliosphere is summarized in the context of the new results from Ulysses. 相似文献
24.
J. Scherrer J. Carrico J. Crock W. Cross A. DeLosSantos A. Dunn G. Dunn M. Epperly B. Fields E. Fowler T. Gaio J. Gerhardus W. Grossman J. Hanley B. Hautamaki D. Hawes W. Holemans S. Kinaman S. Kirn C. Loeffler D. J. McComas A. Osovets T. Perry M. Peterson M. Phillips S. Pope G. Rahal M. Tapley R. Tyler B. Ungar E. Walter S. Wesley T. Wiegand 《Space Science Reviews》2009,146(1-4):35-73
IBEX provides the observations needed for detailed modeling and in-depth understanding of the interstellar interaction (McComas et al. in Physics of the Outer Heliosphere, Third Annual IGPP Conference, pp. 162–181, 2004; Space Sci. Rev., 2009a, this issue). From mission design to launch and acquisition, this goal drove all flight system development. This paper describes the management, design, testing and integration of IBEX’s flight system, which successfully launched from Kwajalein Atoll on October 19, 2008. The payload is supported by a simple, Sun-pointing, spin-stabilized spacecraft with no deployables. The spacecraft bus consists of the following subsystems: attitude control, command and data handling, electrical power, hydrazine propulsion, RF, thermal, and structures. A novel 3-step orbit approach was employed to put IBEX in its highly elliptical, 8-day final orbit using a Solid Rocket Motor, which provided large delta-V after IBEX separated from the Pegasus launch vehicle; an adapter cone, which interfaced between the SRM and Pegasus; Motorized Lightbands, which performed separation from the Pegasus, ejection of the adapter cone, and separation of the spent SRM from the spacecraft; a ShockRing isolation system to lower expected launch loads; and the onboard Hydrazine Propulsion System. After orbit raising, IBEX transitioned from commissioning to nominal operations and science acquisition. At every phase of development, the Systems Engineering and Mission Assurance teams supervised the design, testing and integration of all IBEX flight elements. 相似文献
25.
L. Fletcher B. R. Dennis H. S. Hudson S. Krucker K. Phillips A. Veronig M. Battaglia L. Bone A. Caspi Q. Chen P. Gallagher P. T. Grigis H. Ji W. Liu R. O. Milligan M. Temmer 《Space Science Reviews》2011,159(1-4):19-106
We present an overview of solar flares and associated phenomena, drawing upon a wide range of observational data primarily from the RHESSI era. Following an introductory discussion and overview of the status of observational capabilities, the article is split into topical sections which deal with different areas of flare phenomena (footpoints and ribbons, coronal sources, relationship to coronal mass ejections) and their interconnections. We also discuss flare soft X-ray spectroscopy and the energetics of the process. The emphasis is to describe the observations from multiple points of view, while bearing in mind the models that link them to each other and to theory. The present theoretical and observational understanding of solar flares is far from complete, so we conclude with a brief discussion of models, and a list of missing but important observations. 相似文献
26.
The Electric and Magnetic Field Instrument Suite and Integrated Science (EMFISIS) on RBSP 总被引:2,自引:0,他引:2
C. A. Kletzing W. S. Kurth M. Acuna R. J. MacDowall R. B. Torbert T. Averkamp D. Bodet S. R. Bounds M. Chutter J. Connerney D. Crawford J. S. Dolan R. Dvorsky G. B. Hospodarsky J. Howard V. Jordanova R. A. Johnson D. L. Kirchner B. Mokrzycki G. Needell J. Odom D. Mark R. Pfaff Jr. J. R. Phillips C. W. Piker S. L. Remington D. Rowland O. Santolik R. Schnurr D. Sheppard C. W. Smith R. M. Thorne J. Tyler 《Space Science Reviews》2013,179(1-4):127-181
The Electric and Magnetic Field Instrument and Integrated Science (EMFISIS) investigation on the NASA Radiation Belt Storm Probes (now named the Van Allen Probes) mission provides key wave and very low frequency magnetic field measurements to understand radiation belt acceleration, loss, and transport. The key science objectives and the contribution that EMFISIS makes to providing measurements as well as theory and modeling are described. The key components of the instruments suite, both electronics and sensors, including key functional parameters, calibration, and performance, demonstrate that EMFISIS provides the needed measurements for the science of the RBSP mission. The EMFISIS operational modes and data products, along with online availability and data tools provide the radiation belt science community with one the most complete sets of data ever collected. 相似文献
27.
M. J. Reiner K. A. Anderson E. Roelof T. Armstrong G. B. Hospodarsky J. Fainberg R. G. Stone L. Lanzerotti D. A. Gurnett J. L. Phillips R. Forsyth 《Space Science Reviews》1995,72(1-2):261-266
Both the Ulysses and Galileo spacecraft detected energetic electrons and Langmuir waves that were associated with a type III radio burst on 10 December 1990. At the time of these observations, these spacecraft were in the ecliptic plane and separated by 0.4 AU, with Galileo near the Earth at 1 AU and Ulysses at 1.36 AU. From the measured electron arrival times, the propagation path lengths of the electrons to both Ulysses and Galileo were estimated to be significantly longer than the length of the Parker spiral. These long path lengths are interpreted as due to draping of the interplanetary magnetic field lines around a CME. The onset times of the Langmuir waves at Ulysses and Galileo coincided with the estimated arrival time of the 9 keV and 14 keV electrons, respectively. 相似文献
28.
J.G. Luhmann J.L. Phillips C.T. Russell 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1987,7(12):101-106
The dayside ionospheric magnetic field of Venus has been modelled from two different points of view. The Cloutier et al. electrodynamic model makes specific predictions about the behavior of the global magnetic field configuration that can be compared with those expected from the alternate diffusion/convection model. Although the diffusion/convection model is currently only one-dimensional, it is found that it is consistent with the observations in several areas where the 3-dimensional electrodynamic model is not. 相似文献
29.
A. H. Manson C. E. Meek M. Massebeuf J. L. Fellous W. G. Elford R. A. Vincent R. L. Craig A. Phillips R. G. Roper G. J. Fraser M. J. Smith S. Avery B. B. Balsley R. R. Clark S. Kato T.Tsuda R. Schminder D. Kuerschner 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1990,10(12):267-315
30.
B. E. Goldstein M. Neugebauer J. T. Gosling S. J. Bame J. L. Phillips D. J. Mccomas A. Balogh 《Space Science Reviews》1995,72(1-2):113-116
We report observations of radial and latitudinal gradients of Ulysses plasma parameters. The solar wind velocity increased rapidly with latitude from 0° to 35°, then remained approximately constant at higher latitudes. Solar wind density decreased rapidly from 0° to 35° of latitude, and also was approximately constant beyond that latitude. The mass flux similarly decreased away from the equator (but less than the density), whereas the momentum flux was relatively constant. The radial gradient of the entropy at high latitude indicated a value for the polytrope index of about 1.72 (close to adiabatic); the in-ecliptic estimates of radial gradients for temperature and entropy may be biased by temporal variation. A striking increase in the alpha particle-proton velocity difference with latitude is found. 相似文献