Influence of geometrical form of internal cavity in construction of transversal traction.

Аuthors

Knyazev I. A.

Machinebuilding Design Bureau”Iskra” named after I.I. Kartukov, 35, Leningradskoe shosse, Moscow, 125284, Russia

e-mail: kozlova.iskra@mail.ru

Abstract

This construction can be applied in different directions of development REHF. Presently on the rockets of class «air-to-air» сhange of a vector of a direction reached by turn a flaps. Application of engine of TT on the rockets of «air-to-air» will allow considerably to decrease time of change of vector of direction of rocket, for a few seconds a rocket will be able not only to turn in necessary direction, but also without the special labour will develop on 180º at the minimum radius of turn as a result hit of purpose a rocket probability will grow considerably. Introduction of this construction in a space subject, will allow us to decide the row of problems. One of main problems it is a decline of weight accordingly increase of useful loading. For example, in composition engine installation emergency rescue system (ERS) «Souz-TMA» uses additional engines, which provide thrown down product evade launch vehicle and balance weight which stabilizes flight ERS. Design installation TT on ERS will allow to liquidate additional engines and a balance weight which weighs about 400 kg.

Keywords:

design; mechanism; factor of force of friction; area of enhanceable pressure; calculation area of model; critical section

Download