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Ground control and monitoring of rendezvousThis paper discusses the ground control and monitoring function performed in support of the Gemini rendezvous missions. Included are discussions of the support philosophy adopted for Gemini; the resulting influence upon mission design; and comparisons between predicted and actual flight results.
Document ID
19680005474
Acquisition Source
Johnson Space Center
Document Type
Contribution to a larger work
Authors
Edward L. Pavelka (Johnson Space Center Houston, Texas, United States)
Edgar C. Lineberry (Johnson Space Center Houston, Texas, United States)
Warren J. Kennedy (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
Space Sciences
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
68N14943
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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