Mission to Mars based on the universal small-size platform equipped with an electric propulsion engine-Reference-Cited by-同舟云学术

Mission to Mars based on the universal small-size platform equipped with an electric propulsion engine

Published:2024 Issue:44 Volume: Page:1-32
ISSN:2071-2898
Container-title:Keldysh Institute Preprints
language:
Short-container-title:KIAM Prepr.

Author:

Ovchinnikov Michael Yurievich^ORCID,Korneev Kirill Romanovich^ORCID,Perepukhov Denis Glebovich^ORCID,Mashtakov Yaroslav Vladimirovich^ORCID,Trofimov Sergey Pavlovich^ORCID,Petrukovich Anatoly Alekseevich^ORCID,Korablev Oleg Igorevich^ORCID,Zarubin Dmitry Sergeevich^ORCID,Mamedov Teymur Teymurovich^ORCID,Koshlakov Aleksey Vitaljevich^ORCID,Yudanov Nikolay Anatoljevich^ORCID,Dronov Pavel Alexandrovich¹^ORCID,Nesterenko Alexander Nikitovich¹,Pridannikov Sergey Yurievich¹,Tolstel Oleg Vladimirovich¹^ORCID,Shurshakov Vyacheslav Aleksandrovich^ORCID,Ivanova Olga Alekseevna

Affiliation:

1. JSC Experimental Design Bureau Fakel

Abstract

In the preprint, the concept of a mission to Mars is developed based on the micro-class space platform, a standardized spacecraft with a dry mass of no more than 100 kg equipped with a unified electric propulsion system for orbital maneuvering and attitude control. The spacecraft bus design and the possible payload are described in detail. The preliminary flight dynamics analysis proves the feasibility of the proposed concept.

Publisher

Keldysh Institute of Applied Mathematics

Reference44 articles.

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