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The Science Scenario of the SELENE-2 Mission
Manabu Kato, Kohtaro Matsumoto, Tatsuaki Okada, Satoshi Tanaka, and Science Working Group for Post- SELENE Project
Japan Aerospace Exploration AgencyISAS & ISTA
SELENE-2 Science group is studying:Science goals in lunar scienceCandidate mission and instrumentsCandidate target areaLander-rover designGeophysical study for lunar deep interior using probes
Key questions in lunar science:
(1) Bulk composition of whole moon, and internal structure such as core radius for origin and evolution of the Moon,
(2) Origin of dichotomy, differentiation of magma ocean, and tectonic style for evolution of lunar crust and mantle, and
(3) History of lunar environment such as solar activity and meteoroid impact flux.
・1990 /1/ 24 Launch (M3S-II Rocket)・Orbit Maneuver by Lunar/Solar Gravity Assist Technology of Lunar Orbit Insertion・Technology of Orbit Determination・1993 /4/ 11 Impact on Lunar Surface
JAXA’s Activities in Lunar Exploration
Past
Hiten/Hagoromo
In Development
Lunar-A
SELENE
Under Study
SELENE-2
Technology demonstrationPenetrator mission
Surface remote-sensing
Landing, in-situ observation
SELENE Series Lunar Exploration
• SELENE-1 was defined as a lunar mission for the science of the Moon and demonstration of technology for future exploration of the Moon and planets.
・ Science WG for next lunar mission concluded:
SELENE-2 and after must be landing missions. Candidate mission targets:
1. Geological survey using a science rover.2. Internal structure study using multi-penetrators
(Lunar-B).3. Celestial study using small telescope.4. Sample return for dating and geochemical studies.
Using improved, long-lived penetrators and/or lander,install seismological network for study of lunar internal structure
Investigation of lunar orbital motion by observing polar stars using a celestial telescope
In-situ observation of typical geological features using intelligent rover(s)
Candidate Areas:1. Central peak-type craters
for study of deep crust materials and crater formation
2. Thin crust layer crater such as South Pole Aitken basin for study of mantle materials. ⇔ Moonrise
3. Typical highlands of far-side for highland rock study.
4. Polar regions for exploration of topologically interest area.
Bussey et al. 2005
Lunar North Pole
Central Peak Craters
Tsiolkovsky Crater Clementine UV/VIS ( Pieters & Tompkins (1999))
Gassendi crater
Central peaks: petrologicalinformation of deep crust.Reflectance studies show high contents of
anorthosite in c.p. of both basin and highland areas. (e.g. Tompkins & Pieters(1999))
Remote sensing observation by SELENEIn-situ observation by SELENE-2
CraterCentral Peak
- Multi-band Spectroimager- Gamma-ray Spectrometer- Abrasion・polishing- Sample collection & storage
Geological Analysis Package- Spectromicroscope-X-ray spectro/diffractmeter- Abrasion*polishing
Telescopic imaging spectrometer
- Observation of outcrops in central peak- Temporal surface treatments of samples-In-situ analysis of rocks and soil, major and radioactive elements
-Detailed observations and analyses of rock -samples collected by the rover- Telescopic observations of landing area- Sample transportation from rover to lander
High-resolution imaging of central peak and surroundings
Earth orRelay Sat.
XX--BandBandCMDCMD::1kbps1kbpsTLM:TLM:≧≧2kbps2kbps
S-BandCMD:1kbpsTLM:≧40kbps(LGA) [256kbps(MGA) ]
Broadband: 2Mbps(max)Only Visible-Time
128MB128MB
1GB1GB
128MB128MB
Lander-rover cooperationPayload (including Rover) - 100kg
Pre.Amp.
Φ1.5inch
22--D CCDD CCD
ElectronicsElectronics
XRTXRT
samplesample
XRF, XRD Geophysical
Study Probe
Current Status of Lunar-A
Lunar-A Project has been reviewed by an external review board in JAXA.
Suggestions for improvement were made:1. Assurance of robustness on communication
link between Penetrator and S/C, including the data acquisition during deployment phase.
2. Addition of CPU reset circuit for possiblemalfunction at the impact.
Improvements suggested to the penetrator may take about 3 years, including multiple qualification tests.
Geophysical Study of Lunar Internal Structure:
MantleMantle←←Earth
Thin surface layer Crust
Metal core ?
Th concentration region of lunar surface (Joliff et al.,1998)
◎◎Layer structure study of lunar interiorLayer structure study of lunar interior-- Average density and thickness of lunar Average density and thickness of lunar crustcrust
-- Vertical structure of lunar mantleVertical structure of lunar mantle- Melting feature of lower mantle
- Core density and size◎◎ Heterogeneity study of lunar interior Heterogeneity study of lunar interior structure structure
-- Horizontal distribution of crust Horizontal distribution of crust thicknessthickness
-- Horizontal structure of lunar mantleHorizontal structure of lunar mantle
××
××
××
××Deep moonquake
Seismological observation since Apollo Seismological observation since Apollo missionmissionHeat flow observationHeat flow observationInstallation of wideInstallation of wide--band seismometer band seismometer by by landerlanderEmployment of Employment of penetratorspenetrators carrying carrying short period seismometershort period seismometer
Free oscillationFree oscillation and body wave exited by large moonquake
Detection of Lunar Free Oscillation by LongDetection of Lunar Free Oscillation by Long--period Seismic Recordperiod Seismic Record
Global Survey of Planetary Body InteriorGlobal Survey of Planetary Body Interior
r
( ) ( ) mlr
mlln YrVYrUS 1: ∇+e
( ) rm
lln YrWT e×∇1:
100 S
290 S
101 S
1020 S r
Spheroidal mode
Troidal mode
Free Oscillation Modes:
l = 10, m = 0 l = 10, m = 5
l = 10, m = 10 l = 10, m = 15
Vertical layer contribution to each mode
Technical Development of Long-period Seismometer and Setting Technology
・Carry-on system・Autonomous drilling system
・Alignment・Telecommunication・Operation
Carry-on drilling system on lander
Carry-on long-period seismometerAutonomous drilling and installation of seismometer in subsurfaceAutonomous 3-axis alignment
Bore-holeTypeseismometer
LUNARLUNAR--AA
Body waveSurface wave
FreeOscillation
Earth’s tide
(dig
it/c
m)
(dig
it/c
m)
Frequency characteristics of seismometer
Requirement
Frequency、Hz
STS-1
Autonomous Drilling System
エアバッグを伸縮させて打ちこみ時の反力を支持する案
Air-bag support
Tunnel Boring Machine Mole
Using motor torque
3-axis Alignment Gimbals
Gimbals mechanism onboard Lunar-A penetrator
Heritage of Lunar-A alignment system
Autonomous Gimbals using lunar gravityLight weight and compact
mechanismReduction of shock resistance from
Lunar-A system
The science working group studies;Science mission scenarios,Sampling processes such as crush, polish,abrasion, manipulation under low gravity,In-situ analyses of collected samples by spectrometry of X-ray, Gamma-ray, UV/VISSurvival technology over two-weeks nightsGeophysical probe development; seismometer, heat flow probe, ..
The engineering study working group studies;Pin-point soft landing technology:Navigation, guidance, and hazard avoidance of landerRover technology:Autonomous operation, telecommunication,..Setting mechanism of geophysical probes