european robotic arm (era)wsn.spaceflight.esa.int/docs/factsheets/7 era lr.pdf · → european...
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→ EuropEan robotic arm (Era)
ERA acts as a tool for: Installation, deployment and replacement of elements of the Russian Segment of the Space Station, inspection of the Russian Segment, support/transfer of EVA cosmonauts, transfer of Orbital Replacement Units and other assembly tasks. The arm consists of 2 End Effectors, 2 Wrists, 2 Limbs and 1 Elbow joint together with electronics and cameras. Both ends act as either a “hand” for the robot or the base from which it can operate.
Large relocatable symmetrical robotic arm with 7 degrees of freedom
ERASMUS Centre - Directorate of Human Spaceflight and Operations
PROJECT:
TITLE: ERA DOCUMENT N°:
International Space Station
REV.
2.0ESA-HSO-COU-007
Elbow Camera and Lighting Unit (CLU)
Extra Vehicular Activity handrail
Limb
Camera and Lighting Unit (CLU)
End Effector
PROJECT : SCALE : 1:20
DIMENSIONS : mm
TITLE :European Robotic Arm
DOCUMENT N° :EUC-ESA-FSH-008
International Space Station
Dimensions Total length: 11,300 mm Reach: 9,700 mm Tip position accuracy: 5 mm Maximum tip speed: 100 mm/s Mass budget Launch mass: 630 kg max. P/L handling capability: 8,000 kg Communications infrastructure Power, data and video signals cabling and special fixtures on End Effector and Base Point. Electrical power Average operation power: 475 W (120 V DC) Peak operation power: 800 W (120 V DC) Main construction materials Limb: Carbon fibre tube and Aluminium interfaces Wrist, Elbow and End Effector: Composed of many different materials Thermal Protection: Beta Cloth Blankets Main contractor Dutch Space (Leiden, The Netherlands), leading a consortium of many subcontractors
REV.1.1
Specifications
ERASMUS User Centre and Communication Office
340
348
12284072
Specifications
DImEnSIOnSTotal length: 11,300 mmReach: 9,700 mmTip position accuracy: 5 mm maximum tip speed: 100 mm/s mass budget launch mass: 630 kg max. P/L handling capability: 8,000 kg
COmmUnICATIOnS InfRASTRUCTURE Power, data and video signals cabling and special fixtures on End Effector and Base Point.
ELECTRICAL POwER Average operation power: 475 W (120 V DC) Peak operation power: 800 W (120 V DC)
mAIn COnSTRUCTIOn mATERIALS Limb: Carbon fibre tube and Aluminium
interfaces wrist, Elbow and End Effector: Composed of many different
materialsThermal Protection: Beta Cloth Blankets
mAIn COnTRACTOR Dutch Space (Leiden, The Netherlands), leading a consortium of many subcontractors
TITLE: ERA DOCUMENT N°:
International Space Station
ESA-HSO-COU-007 2.0REV.
PROJECT:
PROJECT : SCALE : 1:20
DIMENSIONS : mm
TITLE :European Robotic Arm
DOCUMENT N° :EUC-ESA-FSH-008
International Space Station
Dimensions Total length: 11,300 mm Reach: 9,700 mm Tip position accuracy: 5 mm Maximum tip speed: 100 mm/s Mass budget Launch mass: 630 kg max. P/L handling capability: 8,000 kg Communications infrastructure Power, data and video signals cabling and special fixtures on End Effector and Base Point. Electrical power Average operation power: 475 W (120 V DC) Peak operation power: 800 W (120 V DC) Main construction materials Limb: Carbon fibre tube and Aluminium interfaces Wrist, Elbow and End Effector: Composed of many different materials Thermal Protection: Beta Cloth Blankets Main contractor Dutch Space (Leiden, The Netherlands), leading a consortium of many subcontractors
REV.1.1
Specifications
ERASMUS User Centre and Communication Office
340
348
12284072
LAUnCH COnfIgURATIOn Launched in so called «Charlie Chaplin» configuration•
with power off Launch vehicle: Proton Launch site: Baikonur Launch date: 2012
On-ORbIT COnfIgURATIOnAttached to different locations on the Russian Segment•Home base: Permanent Multipurpose Module (PMM) •
fLIgHT HARDwARE End Effector with electronics box (2) •Base Points (2 on launcher interface and multiple on ISS) •Wrist (comprising roll, yaw and pitch joints) with joint•
electronics (2)
Utilisation Relevant Data
http://erasmus.spaceflight.esa.int
Illu
stra
tion
s: E
SA/D
. Duc
ros
CLU: Camera and Lighting Units (4) are provided for proximity control and overviews
ImmI: Intra Vehicular Activity Man Machine Interface via a laptop computer
EmmI: Extra Vehicular Activity Man Machine Interface via a control panel
COnTROL InfRASTRUCTURE From the inside of the station with the IMMI via a•
laptop computer and the Control Post Computer From the outside of the station with the EMMI via a•
control panel and the Control Post Computer
Elbow
Joint Electronics
Central Control Computer
Limb 1
Pitch Joint
Yaw Joint Roll Joint
End Effector 1 (EE)
Limb 2 Wrist 2
End Effector 2 (EE)
Base Point with alignment target
EMMI IMMI
Joint Electronics
Elbow Camera and Lighting Unit (CLU)
Wrist 1
Camera and Lighting Unit (CLU)