MMO is the 'Spin-type' spacecraft with the spin rate of 4 seconds.
This is because of the "3-dimensional velocity distribution of particles" and "extension of four long wire antennas (15m)
and two MASTs (5m) for electromagnetic field measurements with centrifugal force".
The spin axis is almost perpendicular to the Mercury equatorial plane.
This is 1) the rejection of solar reflection light into the upper / lower surface of the spacecraft and
2) the continuing aiming of the High-Gain antenna to the Earth with small efforts.
On the side panel, "SSM", a kind of mirror, is fully stuck in order to reflect the much intence sun light.
SSM reflects the optical light and emitts the infrared light, so that
the temperature inside the spacecraft is kept near 'the room temperature'.
(Normal operation of an electric device is not guaranteed at high temperature.)
The MMO spacecraft will enter to the polar orbit with "400km periheam and 12,000km apoherm",
in order to make magnetic field mapping of all spheres and observation of the Mercury magnetosphere in whole regions.
Orbital period is 9.2 hours.
This orbit has the same plane and and 4 times cycle (MPO:2.3 hour) of the MPO orbit,
and can perform cooperation observation with MPO easily.
In the cruise phase to Mercury,
MMO is carried with Mecury Composite System (MCS) under the control of ESA,
jointed with the MPO spacecraft and promotion modules.
After the arrival, the MMO will be separated by spin-ejection,
and be operated by Sagamihara Space Operation Centre in ISAS/JAXA
with UDSC 64m antenna in Nagano Japan.
Payloads for MMO and MPO spacecraft was selected by the international payload review comittee in fall 2004.
Now, several joint payload teams with Japanese and European scientists
actively make design and development efforts.
Moreover, the observation plan after the Mercury arrival will draw up and carry out by the
"BepiColombo Science Working Team" which involved in not only the payload development members
but also the theoretical researchers in both Europe and Japan.
((( MMO Science Working Sub-Group: Payload Teams )))
Name
(member)
Target
PI and Co-PIs
Other Institutions
MGF
(35)
magnetic field
W. Baumjohann (IWF, Austria)
A. Matsuoka (ISAS/JAXA)
Japan: Tokai Univ., Kyushu Univ., Tohoku Inst. Tech.,
Kumamoto Univ., Tokyo Inst. Tech., Univ. Tokyo, NiCT
Europe:Tech. Univ. Braunschweig (Germany)
Imperial College (UK)
Others:APL/JHU, UCLA (USA)
MPPE
(65)
low / high energy
electrons / ions,
energetic neutrals
Y. Saito (ISAS/JAXA)
J.-A. Sauvaud (CESR-CNRS, France)
M. Hirahara (Rikkyo Univ.)
S. Barabash (IRF, Sweden)
Japan: Kyoto Univ., STEL/Nagoya Univ.,
Tokyo Inst. Tech., Tohoku Univ., Univ. Tokyo,
NIPR, NiCT
Europe:
CETP-IPSL, CNRS (France),
MSSL/UCL (UK),
CNR-IFSI (Italy),
Charles Univ., IAP (Czech),
BIRA-IASB (Belgium),
MPS (Germany)
Univ. Bern (Switzerland)
Others: Boston Univ. (USA), National Central Univ. (Taiwan)
PWI
(45)
electric field,
plasma wave,
radio wave
Y. Kasaba (Tohoku Univ.)
J.-L. Bougeret (LESIA, France)
L. Blomberg (Alfven Lab., KTH, Sweden)
H. Kojima (RISH, Kyoto Univ.)
S. Yagitani (Kanazawa Univ.)
Japan: Toyama Pref. Univ., Ehime Univ.,
Kyoto Sangyo Univ., ISAS/JAXA
Europe:
LPCE-CNRS, CETP-IPSL (France),
IRF (Sweden),
Univ. Oslo (Norway),
Finn. Meteo. Inst.,
Univ. Oulu (Finland),
Eotvos Univ. (Hungary),
ESA/RSSD
MSASI
(20)
spectroscopic
image (Na line)
I. Yoshikawa (Univ. Tokyo)
O. Korablev(IKI, Russia)
Japan: Rikkyo Univ., Tohoku Univ.,
Tokyo Polytech. Univ., NIPR, JAXA
MDM
(12)
dust count/moment
H. Shibata (Kyoto Univ.)
Japan:
Tokyo Univ. Marine Sci. Tech.,
Waseda Univ., Osaka City Univ., NAO, ISAS/JAXA
Europe:
MPI-NP (Germany)
<<< MMO model payloads: basis for the project start in 2004>>>
MMO:Payload (2010/11)
Mercury Plasma Particle Experiment
(MPPE)
Mercury Electron Analyzer (MEA)
Low-energy electrons
3eV-30keV, dt=1sec
Mercury Ion Analyzer (MIA)
Low-energy ions
5eV-30keV, dt=2sec
Mass Spectrum Analyzer (MSA)
Ion Mass
5eV-40keV, dt=2sec
High-Energy Ions (HEP-ion)
High energy Particle-Ions
30keV-1MeV,
dt=4sec
High-Energy
Electrons
(HEP-ele)
High energy Particle-electrons
30keV-700keV,
dt=4sec
Energetic Neutrals
Analyzer (ENA)
High-energy Neutral Atoms
<25eV-3.3keV,
dt=80sec
Magnetic Fierld Investigation (MGF)
Magnetic field
DC-64Hz
Plasma Wave Investigation (
PWI)
Electric Field, Plasma wave, Radio wave
DC-10MHz(E)
Few-640kHz(B)
Mercury Sodium Atomosphere Spectral Imager (MSASI)
Na-atmosphere image
FOV:-30deg
Mercury Dust Monitor (MDM)
Interplanetary Dust
PZT