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Title of Article

THE PROBLEMS OF STABILITY OF MOTION OF LAUNCH VEHICLES AND SPACECRAFTS WITH FUEL REDISTRIBUTION


Issue
4
Date
2011

Article type
scientific article
UDC
532.5
Pages
320-321
Keywords
 


Authors
Stepanova Mariya Ilinichna
Gosudarstvennyy kosmicheskiy nauchno-proizvodstvennyy tsentrim. M.V. Khrunicheva, Moskva

Temnov Aleksandr Nikolaevich
MGTU im. N.E. Baumana, Moskva


Abstract
Fuel redistribution, in other words the transfer of fuel from one tank to another, is the solution of some problems in the aviation, rocket and space engineering. One of the ways to improve the power budget of modern heavy-class launch vehicle is to increase the weight efficiency due to the transfer of fuel from one rocket stage tank to another and provide a more complete filling at the separation moment. The novelty of the research is to study the influence of the fuel redistribution on the dynamics of the developed rocket design.

File (in Russian)