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CEV Seat Attenuation System System Design TasksThe Apollo crew / couch restraint system was designed to support and restrain three crew members during all phases of the mission from launch to landing. The crew couch used supported the crew for launch, landing and in-flight operations, and was foldable and removable for EVA ingress/egress through side hatch access and for in-flight access under the seat and in other areas of the crew compartment. The couch and the seat attenuation system was designed to control the impact loads imposed on the crew during landing and to remain non-functional during all other flight phases.
Document ID
20070010702
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Goodman, Jerry R.
(NASA Johnson Space Center Houston, TX, United States)
McMichael, James H.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2007
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: University of Houston, CL, Graduate Class (Capstone)
Location: Houston, TX
Country: United States
Start Date: January 25, 2007
End Date: January 28, 2007
Sponsors: Houston Univ.-Clear Lake
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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