Presentation is loading. Please wait.

Presentation is loading. Please wait.

Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 12 October 2011 г. Программа научных измерений на поверхности.

Published byRolf Miller Modified over 9 years ago

Similar presentations

Presentation on theme: "Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 12 October 2011 г. Программа научных измерений на поверхности."— Presentation transcript:

1 Федеральное космическое агентство НПО 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»

2 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 2 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

3 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 3 Radiator Main Science Deck Solar array Additional Science Deck RITEG Mini Rover (India) RIT Robotic Arm Landers structure (Конфигурация КА) ЛУНА-РЕСУРС / LUNA-RESOURCE

4 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 4 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-GLOB ЛУНА-РЕСУРС / LUNA-RESOURCE

5 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 5 InstrumentMeasurements/Operations Mass (kg) PlaceOrganization Radio-BeaconRadio signal with high stability1,71,7 Main_SDIKI TVRPM (TV for R-Arm) TV imaging of nearest field and objects (for Robotic arm aiming too) 0,5 R_ArmIKI LISIR spectra of minerals1,0 R_ArmIKI Analytic complex Analysis of volatiles content and isotopic ratios 10,4 Main_SD IKI + U.of Bern LASMALaser mass-spectrometer2,8 Main_SD IKI + U.of Bern TV-Spectrometer UV and optical imaging of minerals with UV excitation 0,5 Main_SDIKI ADRON Active neutron and gamma-ray analysis of regolith composition 6,7 Add_SDIKI RAT Radio measurements of temperature of subsurface regolith 0,5 Add_SDIKI PMLMeasurements of dust1,5 Add_SDIKI SEISMOMeasurements of seismic activity1,0 Main_SDIFZ ARIES (L-R only)Measurements of plasma and neutrals2,2 Main_SDIKI TERMO (L-G only) Direct measurements of thermal properties of regolith 0,4 Main_SDGEOKHI LINA (L-G only)Measurements of plasma and neutrals4,6 Main_SD IKI + IFR (Sweden) TV for panorama TV for stereo TV imaging of panoramas and area near Lander (rover and Robotic arm) - Main_SDIKI Retro ReflectorMoon libration and ranging- Main_SDNPO SPP Science payload (Научная аппаратура)

6 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 6 Mission’ scenario (Сценарий миссии)

7 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 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)

8 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 8 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

9 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 9 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=[ о С] for planning

10 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 10 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

11 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 11 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

12 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 12 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

13 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 13 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=[ о С] for planning

14 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 14 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

15 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 15 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

16 Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 16 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)

Download ppt "Федеральное космическое агентство НПО им. С.А. Лавочкина Институт космических исследований РАН 12 October 2011 г. Программа научных измерений на поверхности."

Similar presentations

Институт прикладной математики им. М.В.Келдыша РАН Keldysh Institute of Applied Mathematics, Russian Academy of Sciences.

Институт прикладной математики им. М.В.Келдыша РАН Keldysh Institute of Applied Mathematics, Russian Academy of Sciences.
NASA 2001 Mars Odyssey page 1 Workshop HEND - 2003 Institute for Space Research, June 9 - 11, 2003 BTN – HEND analog on International Space Station (Application.

NASA 2001 Mars Odyssey page 1 Workshop HEND Institute for Space Research, June , 2003 BTN – HEND analog on International Space Station (Application.
Mars Invasion: Spirit, Opportunity, Mars Express Meghan McGovern.

Mars Invasion: Spirit, Opportunity, Mars Express Meghan McGovern.
Instrument Adron-RM for ExoMars 2018

Instrument Adron-RM for ExoMars 2018
ISRO Update Dr. Jayati Datta Programme Manager, Chandrayaan-1 Programme Manager, Space Science Office ISRO HQ Antariksh Bhavan New BEL Road Bangalore 560.

ISRO Update Dr. Jayati Datta Programme Manager, Chandrayaan-1 Programme Manager, Space Science Office ISRO HQ Antariksh Bhavan New BEL Road Bangalore 560.
Payload Site One Upon landing, the LOW prepares for single-site goals and multi-site goals. A drop-box is prepared for single-site goals utilizing various.

Payload Site One Upon landing, the LOW prepares for single-site goals and multi-site goals. A drop-box is prepared for single-site goals utilizing various.
The Lunar Reconnaissance Orbiter (LRO) is the first mission in NASA's Vision for Space Exploration, a plan to return to the moon and then to travel to.

The Lunar Reconnaissance Orbiter (LRO) is the first mission in NASA's Vision for Space Exploration, a plan to return to the moon and then to travel to.
Lunar Advanced Science and Exploration Research: Partnership in Science and Exploration Michael J. Wargo, Sc.D. Chief Lunar Scientist for Exploration Systems.

Lunar Advanced Science and Exploration Research: Partnership in Science and Exploration Michael J. Wargo, Sc.D. Chief Lunar Scientist for Exploration Systems.
The Lander is at a 25 km Lunar altitude and an orbital period of approximately 110 minutes. After separation occurs the Lander is completely self sufficient.

The Lander is at a 25 km Lunar altitude and an orbital period of approximately 110 minutes. After separation occurs the Lander is completely self sufficient.
Project X pedition Spacecraft Senior Design – Spring 2009

Project X pedition Spacecraft Senior Design – Spring 2009
Long Term Science working group status LSWT Venice, 30/03-01/04/2009.

Long Term Science working group status LSWT Venice, 30/03-01/04/2009.
Light and Telescopes Chapter 5. Radio Interferometry The Very Large Array (VLA): 27 dishes are combined to simulate a large dish of 36 km in diameter.

Light and Telescopes Chapter 5. Radio Interferometry The Very Large Array (VLA): 27 dishes are combined to simulate a large dish of 36 km in diameter.
A brief look at previous robotic missions to the moon Presented by Shawn Fenn 9-25-08.

A brief look at previous robotic missions to the moon Presented by Shawn Fenn
Mars Exploration By Jacob Stinar. Water on Mars.

Mars Exploration By Jacob Stinar. Water on Mars.
Mysteries of Earth and Mars Mars Facts and Exploration.

Mysteries of Earth and Mars Mars Facts and Exploration.
Russian Missions to the Moon, Venus, and Mars in the 1960s Vladimir Krasnopolsky Russia was the world leader in space technology at the end of 1950s and.

Russian Missions to the Moon, Venus, and Mars in the 1960s Vladimir Krasnopolsky Russia was the world leader in space technology at the end of 1950s and.
ISRA Introductory - 1 In-Situ Resource Analyzer (ISRA) ISRA is a combined XRF/XRD/Imaging Instrument for Lunar Applications –XRF: X-ray Fluorescence –XRD:

ISRA Introductory - 1 In-Situ Resource Analyzer (ISRA) ISRA is a combined XRF/XRD/Imaging Instrument for Lunar Applications –XRF: X-ray Fluorescence –XRD:
“ PHOBOS - SOIL ” Phobos Sample Return Mission 1. goals, methods of study A.Zakharov, Russian academy of sciences Russian aviation.

“ PHOBOS - SOIL ” Phobos Sample Return Mission 1. goals, methods of study A.Zakharov, Russian academy of sciences Russian aviation.
Final Version Wes Ousley Dan Nguyen May 13-17, 2002 Micro-Arcsecond Imaging Mission, Pathfinder (MAXIM-PF) Thermal.

Final Version Wes Ousley Dan Nguyen May 13-17, 2002 Micro-Arcsecond Imaging Mission, Pathfinder (MAXIM-PF) Thermal.
Page 2Kiruna, 9. Oct 2008, M. Wieser, IRF MEAP/P-BACE launch and flight Martin Wieser Swedish Institute of Space Physics, Kiruna, Sweden and the MEAP/P-BACE.

Page 2Kiruna, 9. Oct 2008, M. Wieser, IRF MEAP/P-BACE launch and flight Martin Wieser Swedish Institute of Space Physics, Kiruna, Sweden and the MEAP/P-BACE.

Similar presentations

Ads by Google