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Title of Article

ANALYZING THE EFFECT OF CONFIGURATION PARAMETERS ON THE STABILITY OF LAUNCH VEHICLES


Issue
4
Date
2011

Article type
scientific article
UDC
532.5.013.4
Pages
248-250
Keywords
 


Authors
Mukhin Aleksey Dmitrievich
Gosudarstvennyy kosmicheskiy nauchno-proizvodstvennyy tsentr im. M.V. Khrunicheva, Moskva


Abstract
A technique for analyzing the stability of launch vehicles analysis is proposed to determine stability thresholds in space of the configuration parameters of a rocket, characterizing the position of tanks with a liquid. The analysis takes into account the effect of these parameters on mass-inertial and dynamic characteristics. Also, the effect of some other key parameters of liquid sloshing and control system on the stability thresholds of a closed-loop system is examined.

File (in Russian)