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Gemini/Agena Docking MechanismThe Gemini/Agena docking mechanisms utilize simple mechanical elements to provide a capability for initial engagement between two orbiting vehicles. The docking mechanisms then rigidize the attachment in a manner suitable for subsequent maneuver with the Agena propulsion system. Finally, the mechanisms provide a capability for disengaging and repeating the entire docking cycle. The mechanical elements used are found in daily terrestrial applications.
Document ID
19660027408
Acquisition Source
Jet Propulsion Laboratory
Document Type
Contribution to a larger work
External Source(s)
https://ntrs.nasa.gov/citations/19660027401
Authors
P H Meyer (McDonnell Aircraft Corporation Saint Louis, Missouri, United States)
Date Acquired
August 3, 2013
Publication Date
May 19, 1966
Publication Information
Publication: Proceedings of the First Aerospace Mechanisms Symposium
Publisher: Proceedings of the First Aerospace Mechanisms Symposium
Subject Category
Space Vehicles
Meeting Information
Meeting: 1st Aerospace Mechanisms Symposium
Location: Santa Clara, CA
Country: US
Start Date: May 19, 1966
End Date: May 20, 1966
Sponsors: Lockheed Martin (United States), Jet Propulsion Lab
Accession Number
66N36698
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Gemini Spacecraft
Docking
Agena docking
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IDRelationTitle19660027401Collected WorksProceedings of the First Aerospace Mechanisms SymposiumN66-36691 22-31Collected Works19660027401Collected WorksProceedings of the First Aerospace Mechanisms Symposium
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