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Penetrators Deployments Robotics
Jerzy Grygorczuk Warsaw, January 2011
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Rosetta mission to the comet
Lander on the comet artistic vision.
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MUPUS-TP onboard PHILAE (ESA-DLR lander)
MANIPULATOR PENETRATOR
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Hammering Device construction
SENSORS ELECTRONICS (ASIC) HAMMER CONTROL ELECTRONICS CAPACITOR 25 µF, 600 V RELUCTANT MAGNETIC CIRCUITRY HAMMER ELASTIC SUSPENSION ROD’S END PLATE
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Penetrator „KRET” (mole)
Elements of the KRET before integration Test set-up
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Tests in a dry sand in 2m test bed
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Technical parameters and performance of the KRET 1
Spring energy [J] Average stroke [mm]
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PHOBOS Sample Return Mission
Lavotchkin manipulator with CHOMIK penetrator
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MUPUS → CHOMIK Stowed configuration During resizing operation
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CHOMIK STM
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Kinetic penetrator (IMPACTOR) for the american mission
Trail Blazer
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Pin-on-Disk Tribometer (ESA PECS project)
Control Unit NI PXI instrumentation platform Instrument
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The novel surface layers for the space mechanisms
Appearance of samples prepared for tribo testing a nitride diffusion layer on Ti6Al4V alloy (b) (c) a nitrided layer on AISI 321 steel and with Ni-P (d) Ni-P-Si3N4 coating on AA7075 aluminum alloy
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NetLander Uprighting Mechanism Sollar arrays deployment
TORQUE: over 100 Nm MASS: 0.9 kg
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Ultralight MANIPULATOR - 3 dof, 3-3.5m, 2kg
Stowed During tilted up extension After full extension and lowering
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