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Joint US/Soviet docking mission.The purpose and objectives of the joint Apollo/Soyuz experimental test flight, the technical requirements and anticipated solutions necessary to meet the objectives, the mission plan, the flight vehicles, the schedule, and the expected results of successfully completing such a project are discussed. The androgynous feature of the docking system is provided by a symmetrical distribution of all elements which are directly connected during docking, relative to the axis of reverse symmetry. Both the American and Russian systems are designed to serve as either the active or passive system for docking and undocking.
Document ID
19730037385
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Scott, D. R.
(USAF, Washington, D.C.; NASA, Manned Spacecraft Center Houston, Tex., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Space Vehicles
Accession Number
73A22187
Distribution Limits
Public
Copyright
Other

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