The invention relates to an end effector device for robot or teleoperated type space vehicle which includes an inflatable balloon member carried on the end of tubular member which has a hollow center or conduit through which a suitable pressurized fluid is supplied. The device may be inserted into a variety of shaped openings or truss-type structures for handling in space.
Pneumatic inflatable end effector
1981-06-16
Miscellaneous
No indication
English
Pneumatic Inflatable End Effector
NTIS | 1978
|PNEUMATIC DE-ICER WITH REDUCED NON-INFLATABLE AREA AT DEICER EDGE
European Patent Office | 2024
|