1. © Lavochkin Association, 2013 Ganymede Lander mission overview

2. © Lavochkin Association. Purposes and main tasks of the space complex 10/2/2015 Ganymede mission 2 Main destination of the space complex, composed of two spacecraft (orbiter and lander) is carrying out of researches of Jupiter and it’s natural satellite Ganymede. The tasks of the orbiter:  entrance to the orbit with the specified parameters around Ganymede;  carrying out of distance researches of the satellite and it’s ambient space;  mapping of the Ganymede surface, selection of landing area for the lander;  transmission to the Earth of scientific data, images of the surface and telemetry data;  retranslation of the data from the lander. The tasks of the lander:  entrance to the orbit with the specified parameters around Ganymede;  carrying out of soft landing to the surface of satellite in preliminary selected area;  carrying out of contact researches of the satellite;  transmission to the orbiter of scientific data, images of the surface and telemetry data (nominal channel);  transmission to the Earth of scientific data, images of the surface and telemetry data (redundant channel).

3. © Lavochkin Association. Initial data 10/2/2015 Ganymede expedition 3 Launch vehicles  separated launch of orbiter and lander with the LV of “Proton”/ “Angara” class;  upper stage– “Breeze-M”;  fairing with diameter of payload zone not less, than 3800 mm. Mass budget  the initial mass of the spacecraft after separation from the upper stage – not less, than 4000 kg;  the mass of the orbiter on entrance to the orbit around Ganymede – not more, than 950 kg;  the mass of the lander after landing to the surface – not more, than 800 kg. Power budget The summary electrical power, provided for all systems of orbiter and lander – not less, than 70 W. Ganymede characteristics  distance to Earth ~ 640 mil. km;  FFA – 0,146g;  orbital velocity – 10,880 km/s;  temperature on the surface – 70…152 K;  surface – ice crust up to 950 km;  atmosphere – none.

4. © Lavochkin Association. Flight scheme into Jupiter system 10/2/2015 Ganymede expedition 4

5. © Lavochkin Association. Flight scheme in Jupiter system 10/2/2015 Ganymede expedition 5 Separation from the cruise module Entering the Ganymede orbit Landing phase Ganymede Europe Maneuver entering the initial orbit Io GM near Ganymede (6) Approaching

6. © Lavochkin Association. Landing scheme 10/2/2015 Ganymede expedition 6 SC orientation

7. © Lavochkin Association. 10/2/2015 Ganymede mission 7 Communication scheme

8. © Lavochkin Association....other parts of SRC Space complex composition 10/2/2015 Ganymede expedition 8 Space complex «Laplace» Space complex «Laplace» Space rocket complex Ground control complex Ground scientific complex Space rocket «Proton» Launch vehicle «Proton» Space head compartment Launch vehicle «Proton» Space head compartment...other parts of SRC Spacecraft «Laplace-O» Spacecraft «Laplace-O» Upper stage «Breeze» Upper stage «Breeze» Transfer module Fairing Spacecraft «Laplace-L» Spacecraft «Laplace-L» Upper stage «Breeze» Upper stage «Breeze» Transfer module Fairing

9. © Lavochkin Association. Orbiter :: version with RTGs 10/2/2015 Ganymede expedition 9 SystemMass, kg Antenna-feeder system65 Board control system55 Telemetry system5 Power supply system160 Propulsion system140 Radio complex15 Structure, cabling, STR145 Reserved mass165 Scientific instruments50 Summary800

10. © Lavochkin Association. Orbiter :: version with solar panels 10/2/2015 Ganymede expedition 10 SystemMass, kg Antenna-feeder system65 Board control system55 Telemetry system5 Power supply system245 Propulsion system140 Radio complex15 Structure, cabling, STR145 Scientific instruments50 Reserved mass220 Summary940

11. © Lavochkin Association. Lander 10/2/2015 Ganymede expedition 11 System Mass, kg Antenna-feeder system 65 Board control system65 Telemetry system5 Power supply system120 Propulsion system215 Radio complex15 Structure, cabling, STR 125 Scientific instruments 50 Mass margin140 Summary800

12. © Lavochkin Association. Systems heritage of orbiter 10/2/2015 Ganymede expedition 12 «Luna-Glob-Orbiter» New development «Luna-Glob», «Luna-recourse» New development

13. © Lavochkin Association. Systems heritage of lander 10/2/2015 Ganymede expedition 13 New development «Luna-Glob» «Luna-Glob», «Luna-recourse» «ExoMars»