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ASCENT ProgramThe ASCENT program solves the three-dimensional motion and attendant structural loading on a flexible vehicle incorporating, optionally, an active analog thrust control system, aerodynamic effects, and staging of multiple bodies. ASCENT solves the technical problems of loads, accelerations, and displacements of a flexible vehicle; staging of the upper stage from the lower stage; effects of thrust oscillations on the vehicle; a payload's relative motion; the effect of fluid sloshing on vehicle; and the effect of winds and gusts on the vehicle (on the ground or aloft) in a continuous analysis. The ATTACH ASCENT Loads program reads output from the ASCENT flexible body loads program, and calculates the approximate load indicators for the time interval under consideration. It calculates the load indicator values from pre-launch to the end of the first stage.
Document ID
20120010446
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
Brown, Richard
(Boeing Co. Houston, TX, United States)
Collier, Gary
(Boeing Co. Houston, TX, United States)
Heckenlaible, Richard
(Boeing Co. Houston, TX, United States)
Dougherty, Edward
(Boeing Co. Houston, TX, United States)
Dolenz, James
(Boeing Co. Houston, TX, United States)
Ross, Iain
(Boeing Co. Houston, TX, United States)
Date Acquired
August 26, 2013
Publication Date
June 1, 2012
Publication Information
Publication: NASA Tech Briefs, June 2012
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MSC-24978-1/9-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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