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Ganymede Lander mission overview

Ganymede Lander mission overview. Purposes and main tasks of the space complex. 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 :

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Ganymede Lander mission overview

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  1. Ganymede Lander mission overview

  2. Purposes and main tasksof the space complex • Main destination of the space complex, composed of two spacecraft (orbiter andlander) 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). Ganymede mission

  3. Initial data • 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. • 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. Power budget The summary electrical power, provided for all systems of orbiter and lander – not less, than 70 W. Ganymede expedition

  4. Flight scheme into Jupiter system Ganymede expedition

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

  6. Landing scheme SC orientation Ganymede expedition

  7. Communication scheme Ganymede mission

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

  9. Orbiter :: version with RTGs Ganymede expedition

  10. Orbiter :: version with solar panels Ganymede expedition

  11. Lander Ganymede expedition

  12. Systems heritage of orbiter New development New development «Luna-Glob-Orbiter» «Luna-Glob», «Luna-recourse» Ganymede expedition

  13. Systems heritage of lander New development New development «Luna-Glob» «Luna-Glob», «Luna-recourse» «ExoMars» Ganymede expedition

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