

SOME ASPECTS OF AERODYNAMIC DESIGNING OF SPACEROCKET SYSTEMS
Kostarev A.A., Kolesnikov A.A.
Samara Space Centre "Progress", Zaporozh'e, Ukraine
Citation:
Kostarev, A.A. and Kolesnikov, A.A., (2011) Some aspects of aerodynamic designing of spacerocket systems, Modern Science: Researches, Ideas, Results, Technologies, Iss. #2(7), PP. 263  268.

Keywords: space transport systems; the launch vehicles; numerical modeling; aerogasdynamics 
Abstracts:
Survey consideration of questions of aerogasdynamics of space transport systems (STS), definitions aerogasdynamics characteristics is conducted. A number of problems in the field of aerogasdynamics with which is short described the designer collides at designing ТКС. Short descriptions of development cycles, the description of problems, methods of the solution, kinds of developed aerodynamic models and experimental researches which are applied to acknowledgement of estimated performance are resulted. The basic aerodynamic characteristics used as initial data for calculation of ballistics of stability and controllability, loads and strength are resulted. Questions of numerical modelling STS are mentioned by means of modern program complexes. 
References:
Петров К.П. Аэродинамика транспортных космических систем.  М.: Эдиториал УРСС, 2000.  368 с.
Краснов Н.Ф. Кошевой В.Н. и др. Аэродинамика ракет.  М.: Высшая школа, 1968.  772 с.


