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Mars pathfinder lander deployment mechanismsThe Mars Pathfinder Lander employs numerous mechanisms, as well as autonomous mechanical functions, during its Entry, Descent and Landing (EDL) Sequence. This is the first US lander of its kind, since it is unguided and airbag-protected for hard landing using airbags, instead of retro rockets, to soft land. The arrival condition, location, and orientation of the Lander will only be known by the computer on the Lander. The Lander will then autonomously perform the appropriate sequence to retract the airbags, right itself, and open, such that the Lander is nearly level with no airbag material covering the solar cells. This function uses two different types of mechanisms - the Airbag Retraction Actuators and the Lander Petal Actuators - which are designed for the high torque, low temperature, dirty environment and for limited life application. The development of these actuators involved investigating low temperature lubrication, Electrical Discharge Machining (EDM) to cut gears, and gear design for limited life use.
Document ID
19960025613
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
Gillis-Smith, Greg R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
August 17, 2013
Publication Date
May 1, 1996
Publication Information
Publication: 30th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
96N27619
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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