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Techniques for Space and Hypersonic Flight Escape (Paracone) Space Systems Center, Douglas Aircraft Company, Incorporated

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Kendall, R. T., author.
Conference Name:
Aerospace Systems Conference and Engineering Display (1967-06-27 : Los Angeles, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1967
Summary:
A single, efficient, reliable emergency escape system is needed to provide, at an acceptable total cost, emergency escape capability throughout the entire mission envelope of hypersonic and orbital vehicles. Analysis and limited testing indicate that the Douglas Paracone emergency escape system will meet this requirement.The Paracone is a gas-inflatable structure shaped like a cone with a large spherical nose. When the cone is deployed , the crew is positioned and supported within the cone approximately one third the length of the cone as measured from the leading edge of the spherical nose. The crew is suspended over an air mattress flotation plenum chamber which, in turn, is located over a gas impact attenuator
Notes:
Vendor supplied data
Publisher Number:
670578
Access Restriction:
Restricted for use by site license

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