2014
DOI: 10.1186/bf03352102
|View full text |Cite
|
Sign up to set email alerts
|

PLANET-B magnetic fields investigation

Abstract: Some scientific topics relating to magnetic field measurements around Mars are briefly described and specification of the magnetic field instrument onboard PLANET-B is presented. The highly elliptical orbit of PLANET-B with a periapsis altitude of 150 km and an apoapsis of 15 R M (Mars radii) will enable us to observe magnetic environments in various regions from the ionospheric altitudes to upstream and tail regions. One of the most important objectives is to resolve the controversial arguments about the magn… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
8
0

Year Published

2018
2018
2020
2020

Publication Types

Select...
5
1
1

Relationship

2
5

Authors

Journals

citations
Cited by 13 publications
(8 citation statements)
references
References 22 publications
0
8
0
Order By: Relevance
“…2.1 Instrumentation LMAG, with a triaxial ring-core type fluxgate sensor (MGF-S), was designed on the basis of magnetometers of two previous missions, Geotail (Kokubun et al 1994) and Nozomi (Yamamoto and Matsuoka 1998). The noise level of peak-to-peak is less than 0.1 nT, and basic specification of LMAG is summarized in Table 1. MGF-S has four dynamic ranges of ±64, ±256, ±1024 and ±65536 nT with a resolution of 16 bits and a linearity better than 0.1% .…”
Section: Instrumentation and Calibrationmentioning
confidence: 99%
“…2.1 Instrumentation LMAG, with a triaxial ring-core type fluxgate sensor (MGF-S), was designed on the basis of magnetometers of two previous missions, Geotail (Kokubun et al 1994) and Nozomi (Yamamoto and Matsuoka 1998). The noise level of peak-to-peak is less than 0.1 nT, and basic specification of LMAG is summarized in Table 1. MGF-S has four dynamic ranges of ±64, ±256, ±1024 and ±65536 nT with a resolution of 16 bits and a linearity better than 0.1% .…”
Section: Instrumentation and Calibrationmentioning
confidence: 99%
“…The MAST for Arase has nearly the same design as that for Nozomi (Yamamoto and Matsuoka 1998) and is similar to those used for Geotail (Kokubun et al 1994), Kaguya (Tsunakawa et al 2010), and BepiColombo MMO, except for the diameter, length, and material used. The MAST was in the stowed configuration at launch, and was deployed about 1 month after launch.…”
Section: -M Extendable Mastmentioning
confidence: 93%
“…The analogtype magnetometer follows the basic design adopted for many space missions (Gordon and Brown 1972;Fukunishi et al 1990;Kokubun et al 1994;Yamamoto and Matsuoka 1998;Tsunakawa et al 2010). Nevertheless, some elements of the sensor and electronics were newly developed to withstand the harsh radiation environment of Mercury (Matsuoka et al 2013).…”
Section: Overviewmentioning
confidence: 99%
“…We also used interplanetary magnetic field (IMF) data. Details of the magnetometer on board Nozomi are described in Yamamoto and Matsuoka (1998). Figure 1 shows the Nozomi orbit projected to the ecliptic plane, where the EarthSun line is fixed in the coordinate.…”
Section: Observationsmentioning
confidence: 99%