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Summary of rendezvous operationsOne of the major objectives of the Gemini Program was to develop and to demonstrate
techniques for the rendezvous and docking of space vehicles. This objective is of vital
importance since rendezvous and docking is mandatory for success in many future
manned space-flight programs. For example, lunar orbital rendezvous has been selected as
the primary mode for the Apollo lunar-landing mission which requires one rendezvous
and two dockings. Other programs requiring rendezvous are planetary missions, manned
space stations, and unmanned satellite inspection and repair missions.
Document ID
19680005473
Acquisition Source
Johnson Space Center
Document Type
Contribution to a larger work
Authors
W. Barnard Evans
(Johnson Space Center Houston, Texas, United States)
Marvin R. Czarnik
(Johnson Space Center Houston, Texas, United States)
Date Acquired
August 4, 2013
Publication Date
February 1, 1967
Publication Information
Publication: Gemini Summary Conference
Publisher: National Aeronautics and Space Administration
Volume: NASA-SP-138
Issue Publication Date: February 1, 1967
URL: https://ntrs.nasa.gov/citations/19680005472
Subject Category
Spacecraft Design, Testing And Performance
Launch Vehicles And Launch Operations
Meeting Information
Meeting: Gemini Summary Conference
Location: Houston, TX
Country: US
Start Date: February 1, 1967
End Date: February 2, 1967
Sponsors: Johnson Space Center
Accession Number
68N14942
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
structural integrity
launch vehicle systems performance
spacecraft systems performance
Gemini spacecraft
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