MARS-OBSERVER MAGNETIC-FIELDS INVESTIGATION

被引:104
作者
ACUNA, MH
CONNERNEY, JEP
WASILEWSKI, P
LIN, RP
ANDERSON, KA
CARLSON, CW
MCFADDEN, J
CURTIS, DW
REME, H
CROS, A
MEDALE, JL
SAUVAUD, JA
DUSTON, C
BAUER, SJ
CLOUTIER, P
MAYHEW, M
NESS, NF
机构
[1] NASA, GODDARD SPACE FLIGHT CTR, GREENBELT, MD 20771 USA
[2] UNIV CALIF BERKELEY, SPACE SCI LAB, BERKELEY, CA 94720 USA
[3] CTR ETUD SPATIALE RAYONNEMENTS, TOULOUSE, FRANCE
[4] GRAZ UNIV, A-8010 GRAZ, AUSTRIA
[5] AUSTRIAN ACAD SCI, SPACE RES INST, GRAZ, AUSTRIA
[6] RICE UNIV, DEPT SPACE SCI, HOUSTON, TX 77251 USA
[7] NATL SCI FDN, WASHINGTON, DC 20550 USA
[8] UNIV DELAWARE, BARTOL RES INST, NEWARK, DE 19716 USA
关键词
D O I
10.1029/92JE00344
中图分类号
P3 [地球物理学]; P59 [地球化学];
学科分类号
0708 ; 070902 ;
摘要
The Mars Observer magnetic fields investigation will provide fast vector measurements of the Martian magnetic field over a wide dynamic range. The fundamental objectives of this investigation are (1) to establish the nature of the magnetic field of Mars, (2) to develop appropriate models for its representation, which take into account the internal sources of magnetism and the effects of the interaction with the solar wind, and (3) to map the Martian crustal remanent field to a resolution consistent with the Mars Observer orbit altitude and ground track separation. The basic instrumentation complement implemented for this mission is a synergistic combination of a dual, triaxial, flux gate magnetometer system and an electron reflectometer with sensors mounted on a spacecraft boom. The dual magnetometer system allows the real-time estimation and correction of spacecraft-generated fields, while the electron reflectometer provides remote magnetic field sensing capabilities. These instruments have an extensive spaceflight heritage, and similar versions of the same have been flown in numerous missions like Vovager, Magsat, International Solar Polar mission (ISPM), Giotto, Active Magnetospheric Particle Tracer Explorers, and Global Geospace Science (GGS). Depending on the telemetry rate supported, a minimum of 2-16 vector samples per second will be acquired. The instrument is microprocessor controlled, can be partially reprogrammed in flight, and supports the packet telemetry protocol implemented for Mars Observer.
引用
收藏
页码:7799 / 7814
页数:16
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