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Mars Pathfinder Lander Deployment MechanismsThe Mars Pathfinder Lander will land, right itself, and open so that none of its airbag covers its solar cells. This requires two different types of mechanisms, the Airbag Retraction Actuators, and the Lander Petal Actuators which are designed for a high torque, low temperature, dirty environment, and limited life application. The development of these actuators investigated low temperature lubrication, Electrical Discharge Machining (EDM) to cut gears, and gear design for limited life use.
Document ID
20210003662
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Gillis-Smith, Greg R.
Date Acquired
May 15, 1996
Publication Date
May 15, 1996
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Mars
Pathfinder
Lander
Deployment
Mechanisms
Actuator

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