NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The Apollo Docking SystemThe Apollo docking system is the means by which the Apollo command and service modules and the lunar module are connected and disconnected during a lunar-landing mission. The system incorporates a CSM probe assembly that mates with a drogue assembly on the LM. Twelve automatic latches mounted on the CSM docking ring provide for structural integrity between the vehicles and for tunnel sealing during crew transfer. A functional description of the flight hardware and the alternate concepts that were evaluated to determine the system best suited to Apollo requirements are presented.
Document ID
19720005743
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kenneth A Bloom
(North American Rockwell Corporation Downey, CA, United States)
George E Campbell
(North American Rockwell Corporation Downey, CA, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1970
Publication Information
Publication: Fifth Aerospace Mechanisms Symposium
Publisher: National Aeronautics and Space Administration
Subject Category
Space Vehicles
Meeting Information
Meeting: Fifth Aerospace Mechanisms Symposium
Location: Greenbelt, MD
Country: US
Start Date: June 15, 1970
End Date: June 16, 1970
Sponsors: National Aeronautics and Space Administration
Accession Number
72N13392
Funding Number(s)
CONTRACT_GRANT: NAS9-150
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available