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Gemini results as related to the Apollo programThe Gemini Program was conceived to provide a space system that could furnish answers to many of the problems in operating manned vehicles in space. It was designed to build upon the experience gained from Project Mercury, and to extend and expand this fund of experience in support of the manned lunar landing program and other future manned space-flight programs. The purpose of this paper is to relate some of the results of the Gemini Program to the Apollo
Program, and to discuss some of the contributions which have been made.

The objectives of the Gemini Program applicable to Apollo are : (1) long-duration flight, (2) rendezvous and docking, (3) post-docking maneuver capability, (4) controlled reentry and landing, (5) flight- and groundcrew proficiency, and (6) extra vehicular capability. The achievement of these objectives has provided operational experience and confirmed much of the technology which will
be utilized in future manned programs. These contributions will be discussed in three major areas : launch and flight operations, flight-crew operations and training, and technological development of subsystems and components. While there is obvious interrelation among the three elements, the grouping affords emphasis and order to the discussion.
Document ID
19680005493
Acquisition Source
Johnson Space Center
Document Type
Contribution to a larger work
Authors
Willis B. Mitchell
(Johnson Space Center Houston, Texas, United States)
Owen E. Maynard
(Johnson Space Center Houston, Texas, United States)
Donald D. Arabian
(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
68N14962
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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