Techniques for Space and Hypersonic Flight Escape (Paracone)

670578

2/1/1967

Authors
Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/670578
Citation
Kendall, R., "Techniques for Space and Hypersonic Flight Escape (Paracone)," Aerospace Systems Conference and Engineering Display, Los Angeles, California, United States, June 27, 1967, https://doi.org/10.4271/670578.
Additional Details
Publisher
Published
2/1/1967
Product Code
670578
Content Type
Technical Paper
Language
English