NASA NTRS · 19670000233
Land landing couch dynamics computer program
Abstract
Computer programs perform landing stability studies of mechanical impact system designs for advanced spacecraft. The programs consider variation in spacecraft vertical and horizontal velocity, attitude and orientation, shock strut load-stroke characteristics, and ground coefficient of friction.
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Herting, D. N., Pohlen, J. C., Pollack, R. A.. 1967-07-01. Land landing couch dynamics computer program. https://ntrs.nasa.gov/citations/19670000233
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