Water landing characteristics of conical shaped capsule employing after-reentry parachute for letdown to water landing; computations for rigid body were made from equations obtained by utilizing principle of conservation of momentum to determine accelerations for flight path of 90° and contact attitude of 0°.
Water-landing characteristics of reentry capsule
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 5-23-59L
1959
27 pages
Report
English
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