12 October 20 11 г

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Федеральное космическое агентствоНПО им. С.А. Лавочкина

Институт космических исследований РАН

12 October 2011 г.

Программа научных измерений на

поверхности Луны

для КА «Луна-Ресурс» и ПсМ «Луна-Глоб»

V. Tretyakov, Space Research Institute, Moscow, Russia

Science investigations on Landers

«Luna-Resource» and «Luna Glob»

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Институт космических исследований РАН Science goals (Научные задачи)

Goal 1: Study of mineralogical, chemical, elemental and isotopic content of regolith and volatiles in polar area of Moon

Goal 2: Study of plasma and dust exosphere of Moon and interaction of space environment with Moon’ surface

Goal 3: Investigation of inner structure of Moon by means of seismic measurements

Задача 1: Исследование состава реголита и физических процессов на лунных полюсах

Задача 2: Исследование свойств экзосферы на лунных полюсах и процессов взаимодействия космической плазмы с поверхностью

Задача 3: Исследование внутреннего строения Луны методами сейсмометрии

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Radiator

Main Science Deck

Solar array

Additional Science Deck

RITEG

Mini Rover (India)

RIT

Robotic Arm

Landers structure (Конфигурация КА)

ЛУНА-РЕСУРС / LUNA-RESOURCE

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Radiator

Main Science Deck

Solar array

Additional Science Deck

RITEG

Mini Rover (India)

RIT

Robotic Arm

Landers structure (Конфигурация КА)

Drilling system

ЛУНА-ГЛОБ / LUNA-GLOBЛУНА-РЕСУРС / LUNA-RESOURCE

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Институт космических исследований РАН Instrument Measurements/OperationsMass (kg)

Place Organization

Radio-Beacon Radio signal with high stability 1,7 Main_SD IKI

TVRPM (TV for R-Arm)TV imaging of nearest field and objects (for Robotic arm aiming too)

0,5 R_Arm IKI

LIS IR spectra of minerals 1,0 R_Arm IKI

Analytic complexAnalysis of volatiles content and isotopic ratios

10,4 Main_SDIKI +

U.of Bern

LASMA Laser mass-spectrometer 2,8 Main_SDIKI +

U.of Bern

TV-SpectrometerUV and optical imaging of minerals with UV excitation

0,5 Main_SD IKI

ADRONActive neutron and gamma-ray analysis of regolith composition

6,7 Add_SD IKI

RATRadio measurements of temperature of subsurface regolith

0,5 Add_SD IKI

PML Measurements of dust 1,5 Add_SD IKI

SEISMO Measurements of seismic activity 1,0 Main_SD IFZ

ARIES (L-R only) Measurements of plasma and neutrals 2,2 Main_SD IKI

TERMO (L-G only)Direct measurements of thermal properties of regolith

0,4 Main_SD GEOKHI

LINA (L-G only) Measurements of plasma and neutrals 4,6 Main_SDIKI +

IFR (Sweden)

TV for panoramaTV for stereo

TV imaging of panoramas and area near Lander (rover and Robotic arm)

- Main_SD IKI

Retro Reflector Moon libration and ranging - Main_SD NPO SPP

Science payload (Научная аппаратура)

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Институт космических исследований РАН Mission’ scenario (Сценарий миссии)

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1. Flight to Moon and landing (Перелет до Луны и посадка)

2. After landing commissioning (Этап диагностирования и

тестирования аппаратуры после посадки)

3. Minimal success of mission (Выполнение задач для обеспечения

минимального успеха миссии)

4. Operation on sunset (Работа на закате)

5. Preparation to night (Переход к ночи)

6. After night commissioning (Этап диагностирования и

тестирования аппаратуры после ночи)

7. Operation (Штатная работа в течение основного и

дополнительного сроков миссии)

8. Close of mission (Завершение миссии)

Main stages (Основные этапы)

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1. Flight to Moon

2. Background measurements (ADRON, RAT, PML, other -?)

3. Landing (no science operation except TV!).

1. Flight to Moon and landing (Перелет до Луны и посадка)

Goal – devices test after launch, background measurements

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1. SC systems tests + charging

2. TV-panorama и TV-stereo

3. Mini Rover tests (на L-R)

4. Robotic Arm test (+ Drilling system for L-G)

5. BUNI tests

6. Other devices tests (depend on power)

2. After landing commissioning (Диагностирование аппаратуры после посадки)

Goal– devices test after landing, correction of cyclograms according

to real parameters P=[Wt], I=[Mb], Т=[оС] for planning

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REM 1: T= (Sundown - N earth days) depend on landing site and power needs for

night surviving. N 1

1. TV panorama and TV shooting for circumstances (1).

2. Mini Rover operation start (for L-R)

3. Testing Area selection for TVRPM and LIS.

4. Testing Area excavation by means Robotic Arm

5. TV shooting of Testing Area from TVRPM and LIS.

6. Delivery the sample of regolith by Robotic Arm to Chromatograph and LASMA

7. Analysis the sample of regolith by Chromatograph and LASMA

8. Repetition the TVRPM and LIS shooting of Testing Area up to time T,

where T=Sundown - N earth days (see Rem. 1)

9. Operation of monitoring device (ARIES, ADRON, SEISMO, TVKS, RAT, PML), TERMO (on L-G) and RADIOBEAKON up to T.

3. Minimal success of mission (Обеспечение минимального успеха миссии)

Goal– minimal set of science measurements

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1. Stop science operation for time T.

2. Battery charging to 100%

3. BUNI turn on

4. Operation of ARIES, SEISMO, TVKS, RAT, PML, TERMO (on L-G)

5. Measurements during Y hours (see Rem. 2)

6. Data downlink on Earth

7. Science devices and BUNI turn off

4. Operation on sundown(Работа на закате)

Goal– safe operation and measurement before and after sundown

REM 2: Y depend on power!

REM 1: T (=Sundown - N earth days) depend on landing site and power needs for

night surviving. N 1

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1. Parking of Robotic Arm and Drilling System

2. Charging to 100%

3. TM data downlink on Earth

4. Science devices and BUNI turn off

5. Preparation to night(Переход к ночи)

Goal– safe transition to night regime

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1. Charging to 100% + SC systems tests

2. Robotic Arm tests (+ Drilling system tests for L-G)

3. TVRPM and LIS tests

4. BUNI test

5. Science devices turn on and tests

6. After night commissioning (Диагностирование аппаратуры после ночи)

Goal– tests after night , correction of cyclograms according to real

parameters P=[Wt], I=[Mb], Т=[оС] for planning

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1. Wake up after night.

2. TV panorama and TV stero shooting circumstance.

3. TV shooting of Testing Area from TVRPM and LIS

4. Shooting of closes landscape from TVRPM и LIS of SC

5. Drilling system operation for sample of regolith from depth

6. Robotic Arm delivery of sample of regolith to Chromatograph and LASMA

7. Sample of regolith analysis by Chromatograph and LASMA

8. Operation of monitoring device (ARIES, ADRON, SEISMO, TVKS, RAT, PML),

TERMO (on L-G) and RADIOBEAKON up to T=Sundown - N earth days

9. Preparation to Power Off mode during night

7. Operation (Штатная работа)

Goal– routing science measurements

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1. Science devices turn off

2. PADIOBEACON turn to RITEG power

3. BUNI turn off

4. SC turn off

8. Close of mission (Завершение миссии)

Goal – end of operation and start the support of future

mission by means of beacon radio signal

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1. Program of science investigation during mission

2. Base set of cyclograms for operation on Moon.

3. Software for illumination and up/down radio link condition on landing

site («Moon-Environment»).

4. Software for planning of device operation on Moon («Moon-Operation»).

5. On-Earth science experiment support segment (Hardware + «Moon-

Environment» + «Moon-Operation» + Inetrnet + DataBase + Lasers + so

on)

6. Tests and verification of device operation during on-earth (pseudo data

and pseudo telemetry; hardware/software tests, cyclograms

verification, failure mode analysis)

Tasks (Задачи)

Documents

12 October 20 11 г