Development of X-15 escape systemThe content of this paper is concerned primarily with testing and determining the suitability of such factors as cockpit mobility, escape potential, mechanical reliability, post-separation performance, and airframe compatibility. Integrating the results of the various studies led to the conclusion that the pressure suit in combination with the open ejection seat would best satisfy the X-15 emergency-escape requirements by virtue of elimination of capsule-imposed penalties on aircraft performance and significant reduction in development time.
Document ID
19930092389
Acquisition Source
Legacy CDMS
Document Type
None
Authors
Hegenwald, J F
Date Acquired
August 15, 2013
Publication Date
July 30, 1958
Accession Number
93R21679
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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Related Records
IDRelationTitle19930092380Collected WorksResearch-Airplane-Committee Report on Conference on the Progress of the X-15 Project : A Compilation of the Papers Presented