Choice of parametres of penetrator for research of a lunar ground

Аuthors

Rodchenko V. V.^*, Sadretdinova E. R.^**, Gusev E. V.^***

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: dekanat6@cosmos.com.ru
**e-mail: elnara-5@mail.ru
***e-mail: kafedra610@yandex.ru

Abstract

The project «Moon-Glob» urged to investigate internal structure of the Moon. For realisation of this project it is necessary to solve a problem of introduction ofpenetrators in a lunar ground on depth of several metres. In article questions of a choice ofparametres of penetrators for movement in the lunar ground, using as a power-plant the rocket engine of firm fuel are stated. Questions oj improvement of taktiko-technical characteristics by use of devices of various constructive decisions are considered.

Keywords:

the rocket engine of firm fuel, penetrator, movement in a lunar ground, modeling, the mathematical model