Methodology of designing a space transport system including a 'DM' chemical upper stage and an electric rocket transport module

Autor: A. S. Russkikh, V. V. Salmin

Publikováno v: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 21, Iss 4, Pp 66-75 (2023)

The article is devoted to the development of a methodology for designing a space transport system that has, in comparison with traditional injection scenarios, higher characteristics of the mass of the payload to be launched into high-energy orbits,

Externí odkaz: https://doaj.org/article/f710860172594cc59131416b99eca388

Development of the combined method to de-orbit space objects using an electric rocket propulsion system

Autor: Golubek, Aleksandr, Dron’, Mykola, Dubovik, Ludmila, Dreus, Andrii, Kulyk, Oleksii, Khorolskiy, Petro

Publikováno v: Східно-Європейський журнал передових технологій; Том 4, № 5 (106) (2020): Прикладна фізика; 78-87
Восточно-Европейский журнал передовых технологий; Том 4, № 5 (106) (2020): Прикладная физика; 78-87
Eastern-European Journal of Enterprise Technologies; Том 4, № 5 (106) (2020): Applied physics; 78-87

A method has been developed for the combined de-orbiting of large-size objects of space debris from low-Earth orbits using an electro-rocket propulsion system as an active de-orbiting means.A principal de-orbiting technique has been devised, which ta

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=scientific_p::c59aefb66eab35d7497f907eae9f66ab
http://journals.uran.ua/eejet/article/view/210378