Model tests have been made to determine the landing-impact characteristics of a parachute-supported reentry capsule that had a compliable metal structure as a load-alleviating device. A 1/6-scale dynamic model having compliable aluminum-alloy legs designed to give a low onset rate of acceleration on impact was tested at flight-path angles of 90 degrees (vertical) and 35 degrees, at a vertical velocity of 30 ft/sec (full scale), and at contact attitudes of 0 degrees and +/-30 degrees. Landings were made on concrete, sand, and water.
Effect of Load-Alleviating Structure on the Landing Behavior of a Reentry-Capsule Model
1961-03-13
Audio-visual
No indication
English
Landing of a Manned Reentry Capsule: the Ground Population Safety Aspects
British Library Conference Proceedings | 1994
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