MISSION DESIGN OF ADAPTING MARS ENTRY, DESCENT AND LANDING SYSTEM FOR EARTH: RITD-PROJECT

被引：0

作者：

Koryanov, Vsevolod ^{[1
]}

Kazakovtsev, Victor ^{[1
]}

Toporkov, Alexey ^{[1
]}

机构：

[1] Bauman Moscow State Tech Univ, 2nd Baumanskaya Str,5,Build 1, Moscow 105005, Russia

来源：

THIRD IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2017 | 2017年 / 161卷

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The task motion of the spacecraft in the atmosphere is a complex and very important to carry out the planned mission. For the design of such a mission it has developed a special technology for the descent of the spacecraft in the atmosphere of the planet. This technology is based on the concept of using inflatable braking devices and was originally developed for landing in conditions of Mars. Idea of this project - to assess the possibility and the advantage this technology for use in a descent into the Earth's atmosphere to deliver payloads of small size with low-Earth orbits.

引用

页码：691 / 699

页数：9

共 6 条

[1]

Aleksashkin S.N., 2012, HERALD FEDERAL STATE, V2, P4

[2]

Harri A.-M., ADAPTING MARS ENTRY

[3] Longitudinal stability analysis of a suborbital re-entry demonstrator for a deployable capsule [J].

Iacovazzo, Michele ;

Carandente, Valerio ;

Savino, Raffaele ;

Zuppardi, Gennaro .

ACTA ASTRONAUTICA, 2015, 106 :101-110

[4]

[Казаковцев Виктор Поликарпович Kazakovtsev V.P.], 2012, [Вестник Московского государственного технического университета им. Н.Э. Баумана. Серия: Машиностроение, Herald of the Bauman Moscow State Technical University. Mechanical Engineering, Vestnik Moskovskogo gosudarstvennogo tekhnicheskogo universiteta im. N.E. Baumana. Seriya: Mashinostroenie], P39

[5]

Koryanov V., 2013, P INT ASTR C IAC, V8, P5831

[6]

Koryanov V., 2014, P INT ASTR C IAC, V8, P5628

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