Main design characteristics of small scientific and applied-purpose spacecraft based on the Aist-2 unified platform-Reference-Cited by-同舟云学术

Main design characteristics of small scientific and applied-purpose spacecraft based on the Aist-2 unified platform

Published:2020-12-15 Issue: Volume: Page:5-20
ISSN:2308-7625
Container-title:Space engineering and technology
language:ru
Short-container-title:

Author:

KIRILIN Aleksandr N.¹,AKHMETOV Ravil N.²,BAKLANOV Aleksandr I.²,STRATILATOV Nikolay R.²,ABRASHKIN Valeriy I.¹,KOSMODEMYANSKY Evgeniy V.³,SALMIN Vadim V.¹,TKACHENKO Ivan S.¹,SAFRONOV Sergey L.¹

Affiliation:

1. Samara National Research University

2. Joint Stock Company Space Rocket Center Progress

3. Experimental design bureau Fakel

Abstract

The description of the unified platform of small spacecraft AIST-2 is presented. The platform is intended to accommodate various types of science equipment, Earth remote sensing equipment and onboard support systems. The description of the unified platform design, main onboard systems, ground control facilities, data acquisition and processing is given. The results of design studies, construction and operation of small spacecraft built on the basis of the AIST-2 unified platform are presented. The design, onboard composition, technical characteristics and results of operation of the first small spacecraft in the line – AIST-2D which it was launched on April 28, 2016 in the scope of the first launch campaign from the Vostochny Cosmodrome by the Soyuz-2.1a launch vehicle with the Volga ascent unit are described in detail. The results of design studies on the development of advanced small spacecraft based on the AIST-2 platform capable of functioning as part of the space monitoring system are described. Key words: small spacecraft, unified platform, design configuration, remote sensing of the Earth, stereoscopic image equipment, electro-rocket propulsion system.

Publisher

RSC Energia

Reference14 articles.

1. Reference

2. 1. Steimlea C., Gaucheb J.-F., Ernstc H., Tourneurd C. Airbus new payload hosting and end-to-end mission concepts. 68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, 2017, vol. 15, pp. 9689–9694.

3. 2. GOST 4784-97. Alyuminii i splavy alyuminievye deformiruemye. Marki [Aluminium and wrought aluminium alloys. Grades]. Moscow, Standartinform publ., 2009. 31 p.

4. 3. Kirilin A.N., Akhmetov R.N., Shakhmatov E.V., Tkachenko S.I., Baklanov A.I., Salmin V.V., Semkin N.D., Tkachenko I.S., Goryachkin O.V. Opytno-tekhnologicheskii malyi kosmicheskii apparat «AIST-2D» [Experimental technological small spacecraft AIST-2D]. Samara: SamNTs RAS publ., 2017. 324 p.

5. 4. Avanesov G.A., Bessonov R.V., Forsh A.A., Kudelin M.I. Analiz sovremennogo sostoyaniya i perspektiv razvitiya priborov zvezdnoi orientatsii semeistva BOKZ [Analysis of the current state and development prospects of stellar orientation devices of the BOKZ family]. Izvestiya vuzov. Priborostroenie, 2015, vol. 58, no. 1, pp. 3–13.

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