Симпозиум Исследования Солнечной системы

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Производство гамма и нейтронного излучения в приповерхностном слое Production of gamma and neutron radiation in the subsurface Определение элементного состава поверхности по гамма линиям Analysis of elemental composition through detection of gamma lines

Поиск воды по данным измерений нейтронного альбедо Search of water from measurements of neutron albedo Neutron spectrum 10% H 2 O 0% H 2 O Эпитепловые и быстрые нейтроны Epithermal and fast neutrons 1% Н 2 О Тепловые нейтроны Thermal neutrons Energy, MeV

Missions with nuclear spectroscopy instruments

Name Ranger missions/usa Missions with nuclear spectroscopy instruments Luna-10/USSR Luna-12/USSR Apollo-15/USA Apollo-16/USA Venera-8/USSR Venera-9/USSR Venera-10/USSR Time Frame Early 1960s 1966 1971-1972 1972-1975 Planet Body Moon Moon Moon Venus (landing module) Instruments NaI(Tl) Scintillation gamma spectormeters NaI(Tl) Scintillation Gamma-ray spectrometer NaI(Tl) Gamma-Ray spectrometer HP Ge Gamma spectrometer Results Measurements of cosmic gamma ray background and gamma-spectra from Moon surface Measurements of cosmic gamma ray background and gamma-spectra from Moon surface Mapping (Altitude ~ 100-120 km, covering of ~20% of Moon surface) of elemental composition (including Fe Th, and Ti) Measurements of gamma lines form radioactive elements Th, U, K at the landing sites Mars-5/USSR 1974 Mars NaI(Tl) Gamma-Ray spectrometer Abundance of O, Si, Fe, U Th and K in the equatorial regions of Mars (elliptical orbits around Mars with periapsis ~ 1760 km) Vega-1/USSR Vega-2/USSR 1985 Venus (landing module) CsI(Tl) Gamma-Ray spectrometer Measurements of gamma lines form radioactive elements Th, U, K at the landing sites Phobos/USSR 1988 Mars and Phobos CsI(TL) Gamma-Ray spectrometer Abundance of O.Si, Fe, K and Th in the equtorial regions of Mars (two elliptical orbits around Mars with periapsis ~ 900 km) Mars Observer/USA 1992 Mars HP Ge Gamma spectrometer and plastic neutron detector Failed prior Mars orbit insertion Mars-96/Russia 1996 Mars HP Ge Gamma spectrometer Failed prior insertion to the interplanetary orbit NEAR/USA 1996 NaI(Tl) [with BGO Eros asteroid Симпозиум anticoincidence Исследования shield] Солнечной Abundances системы for O,MG,Si,Fe and K Gamma-Ray spectrometer

Name Time Frame Planet Body Instruments Results Missions with nuclear spectroscopy instruments Lunar Prospector/ USA 1998 Moon BGO gamma ray spectrometer + boron plastic and 3 He proportional counters as neutron detectors Mapping of elemental composition of Moon surface including Hydrogen at polar regions (with spatial resolution ~60km) Mars Odyssey/USA 2001- Mars HP Ge Gamma spectrometer + plastic scintillator as neutron spectormeter + High Energy Neutron Detector (Russia) Mapping (Altitude ~ 400 km) of elemental composition of major and radioactive elements, Discovery of water ice in the high-latitude regions, observation of mars seasonal CO2 cycle MESSENGER/USA 2004- Venus (landing module) HP Ge Gamma spectrometer + boron loaded plastic neutron detectors On his way to Mercury (To perform maps of elemental composition + search for water ice) Dawn/USA 2007- Vesta and Ceres CdZnTe and BGO Gamma-Ray spectrometer+boron loaded plastic neutron detectors On his way to asteroids (To get global maps of major and radioactive elements and ice, circular polar orbits around each asteroids) Selene/Japan 2007- Moon HP Ge Gamma spectrometer On his way to the Moon (To get global maps of major and radioactive elements, polar circular orbit with altitude ~100km) LRO/USA 2008- Collimated neutron Under preparation (To get abundance of detector LEND (provided MoonСимпозиум Исследования Солнечной H at the системы polar regions of Moon with spatial by Russia) based on 3He resolution ~10km) proportional counters

Name Time Frame Planet Body Instruments Results MSL/USA 2009- Phobos- Grunt/Russia BepiColombo/ESA 2009-2013- Mars Phobos Mercury Active neutron logging Under preparation (To get depth along the path of rover distribution of bound water along the path (DAN instrument provided of MSL rover) by Russia) LaBr 3 gamma spectrometer + neutron spectrometer based on 3He tubes and Stilben cristal LaBr 3 gamma spectrometer + neutron spectrometer based on 3He tubes and Stilben cristal (Provided by Russia) Under preparation (To get abundances of major and radioactive elements including H at the landing site) Under preparation (to get maps of major and radioactive elements and H abundances at polar cold traps)

Lunar Prospector Results

Prettyman et al., 2006

Prettyman et al., 2006

Prettyman et al., 2006

Water ice remnants? Feldman et al., 2001

Mars Odyssey Results

HEND instrument onboard Mars Odyssey: Main Results Gamma Sensor 2001 Mars Odyssey NS HEND HEND instrument onboard Mars Odyssey: More than four years on Martian orbit. More than two Martian years of mapping of Martian surface. Continuous observation of neutron albedo of Mars in wide energy range. Discovery of subsurface water ice distribution in polar regions and long term monitoring of Martian seasonal caps.

HEND instrument onboard Mars Odyssey: Main Results 60 60 HEND instrument onboard Mars Odyssey: Main results С Ю нейтроны, отсчеты/сек

Observations of seasonal variations of neutron flux produced in Martian subsurface: monitoring of growth and sublimation of seasonal caps Southern he misphere Summer Winter

Fall Winter Spring Summer 50S-60S 60S-70S 70S-80S 80S-90S

HEND instrument onboard Mars Odyssey: Main Results Mass of northern seasonal cap HEND Mass 60N-90N HEND instrument onboard Mars Odyssey: Main results GRS Mass 60N-90N, (Kelly et al., 2007) Gravity Mass, (Karatekin et al., 2006) GCM Mass 56N-90N

HEND instrument onboard Mars Odyssey: Main Results Mass of southern seasonal cap HEND (averaged for several years) Mass (kg) Gravit. Models (Karatekin et al., 2006) GRS GCM

Boynton et al, 2007 Preliminary GRS elements abundance maps

Future Missions

LRO Instruments: LEND South LRO Mission Requirement The LRO shall obtain high spatial resolution hydrogen mapping of the Moon's surface to a 20% accuracy and 5 km resolution at the poles. The LRO shall identify putative deposits of appreciable surface or near surface water ice in the Moon s polar cold traps at 100m scale spatial resolution The LRO shall characterize the deep space radiation environment in lunar orbit, including neutron albedo. North LEND Data Products The content of Hydrogen in subsurface at polar regions with spatial resolution from 5 km (Half-Width Half-Maximum) and with variation sensitivity from 100 parts per million (ppm) The water ice column density on polar regions of the Moon with spatial resolution from 5-20km. Global distribution of neutrons at Moon s orbit with spatial resolution of 50 km at different energy ranges from thermal energy up to >15 MeV separately for periods of quiet Sun and for periods of Solar Particle Events.

LRO Instruments: LEND Instrument parameter Mass (with MLI, kg) Sizes (mm) Operational power (W) Heating power (W) Telemetry rate Total daily telemetry Number of commands Energy ranges of neutron measurements Time resolution (sec) Spatial resolution (@50 km) Рисуно к 1 Figure Thermal neutrons < 0.4 ev, Epithermal neutrons 0.4 ev 10 kev, Fast neutrons 10 kev 1 MeV; High energy neutrons 1.0 MeV-15MeV 1 Value 23.7 460 x 460 x 438 9.5 3.5 3 kbps 250 Mb 7 >1.0 Radius 5 km Provider: Space Research Institute, Russia

MSL Instruments: DAN MSL Mission Requirement To perform either at least 10 5 monitoring measurements of H content with sensitivity or 1 wt% (water equivalent), or at least 500 measurements of H content with high sensitivity of 0.1 wt% (water equivalent) DAN Data Products The depth distribution of Hydrogen in subsurface (down to 0.5 m) along the trace of MSL with spatial resolution from 0.5 meter to tens of meters To measure neutron component of radiation environment during the period of quiet Sun and during Solar Particles Events The fluxes of thermal and epithermal neutrons along the trace of MSL with for periods of quiet Sun and for periods of Solar Particle Events.

PARAMETER DAN/DE DAN/PNG 0.008 0.007 Mass 1.9 kg + 0.2 kg 2.7 kg + 0.1 kg 0.006 0.005 Power <3.5 W <12 W 0.004 0.003 Max Dimensions 204 x 61 x 210 mm 125 x 45 x 339 mm 0.002 0.001 Functions Neutron detection Neutron emission 0.000 10 0 10-1 10-5 10-4 10-3 10-2 Energy Band Thermal and epithermal neutrons in wide energy range Fast neutrons with energy = 14 MeV in pulses 1-2 µs with 10 7 particles Countin g rate 10-2 10-3 10-4 10-5 10-6 10-7 10-8 W ater, w gt% 0% 0.1% 0.3% 0.5% 1.0% 3.0% 5.0% 10.0% 15.0% 20.0% 25.0% 99.0% Temporal resolution Spatial Horizontal resolution Vertical resolution 10-1000 µs < 1 m 1 m <1 µs < 1 m 1 m 10-7 10-6 10-5 10-4 10-3 10-2 Life time 5 years 3 years and/or 10 7 neutron pulses Provider: Space Research Institute, Russia

Phobos-Grunt Instruments: NS HEND NS-HEND: main characteristics Science objectives: Abundances of hydrogen, major and radioactive elements PARAMETER Mass Power Volume Time Resolution Energy range, neutrons Energy range, gamma Temperature range Detectors Position Altitude VALUE 3,8 kg 6 W > 0.25 sec Multi energy bands covering 0.4 ev 15MeV Multi energy bands covering 30 kev 10 MeV (-40C, 40C) 3He proportional counters, stilben crystal, LaBr3 crystal Phobos Grunt Phobos surface NS HEND

BepiColombo Instruments: MGNS MGNS: main characteristics Science objectives: Mapping of major and radioactive elements, search for Hydrogen in polar cold traps PARAMETER Mass Power Volume Surface Resolution Time resolution Energy range, neutrons Energy range, gamma Energy resolution, gamma Detectors Temperature range Position Altitude VALUE 5.2 kg 5 W - 400 km 20 sec Multi energy bands covering 10-3 ev 15 кev 300 kev 10 MeV 3% at 662 kev 3He proportional counters, stilben crystal, LaBr 3 crystal (-20C, 40C) ESA: BepiColombo 400 km 1500 km