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Investigation Of Propellant Actuated Devices For Use In Emergency Crew Escape Systems For Advanced Aerospace Vehicles. Phase III. Design Study.
Author(s): Bleikamp, R. H., Lake, E. R., McGovern, D. R.
Corporate Author(s): McDonnell Aircraft Corp St Louis MO
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-04
Report number: AFFDL TR 65-26 Part 2

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