This article may be expanded with text translated from the corresponding article in Russian. (November 2020) Click [show] for important translation instructions.
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It is being developed within the framework of the federal target program "Creation of a super-heavy class space rocket complex for 2020-2030"[1] and the program cost is estimated at 1.5 trillion roubles (US$1.6 billion). It is the main rocket of the Russian Lunar program.
The final design for the rocket was expected to be complete by autumn 2021,[2] but the program appears to have been paused or stopped just before this expected completion date.
2026-2028 - construction and commissioning of infrastructure for a super-heavy launch vehicle and a medium-class rocket for launching crewed spacecraft from the Vostochny cosmodrome.[6]
Design
The first stage will consist of 6 blocks, each block will be based on the first stage of the planned Irtysh / Soyuz-5 rocket with an RD-171MV engine.[7]
Anatoly Zak
RussianSpaceWeb.com
Roadmap with two rockets on the right Yenisei and Don respectively
"Irtysh" "Soyuz-5" is a basis for the first stage
"Volga" "Soyuz-6" will be used as a basis for second stage
"Yenisei"
"Yenisei" (cutaway)
"Don"
The second stage will consist of one block - matching the first stage of Soyuz-6 - with RD-180 as engine.[7]
Flight tests of a super-heavy launch vehicle will take place in two stages from 2028 to 2035.[11]
The first stage of testing will take place in 2028–2032. It involves the launch of a crewed spacecraft, a lunar take-off and landing complex (LVPK) and other payloads on the trajectory of the flight around the Moon and circumlunar orbits in order to work out the elements of a crewed complex, create a station in the orbit of the Moon, and land on the lunar surface.
The second stage of testing will take place in 2032–2035. It is planned to launch LVPK and other uncrewed payloads for the construction and operation of a base on the lunar surface. In addition, this stage involves participation in international programs related to the study of Mars.
Applications
The super-heavy rocket is supposed to be used in the Russian lunar program, since the carrying capacity of the Angara-A5V launch vehicle (37.5 tons to LEO) is insufficient for these purposes.
^ ab"Transformation of Roscosmos". Russki Kosmos. 7: 2–7. July 2019.
^"RSC Energia: flight tests of the Soyuz-5 rocket will take place from 2022 to 2025 (In Russian)". TASS. 3 July 2018.
January 06, 2023
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This article may be expanded with text translated from the corresponding article in Russian November 2020 Click show for important translation instructions Machine translation like DeepL or Google Translate is a useful starting point for translations but translators must revise errors as necessary and confirm that the translation is accurate rather than simply copy pasting machine translated text into the English Wikipedia Consider adding a topic to this template there are already 2 703 articles in the main category and specifying topic will aid in categorization Do not translate text that appears unreliable or low quality If possible verify the text with references provided in the foreign language article You must provide copyright attribution in the edit summary accompanying your translation by providing an interlanguage link to the source of your translation A model attribution edit summary is Content in this edit is translated from the existing Russian Wikipedia article at ru Enisej raketa nositel see its history for attribution You should also add the template Translated ru Enisej raketa nositel to the talk page For more guidance see Wikipedia Translation Yenisei Russian Enisej project name RN STK 1 Raketa Nositel SverkhTyazhologo Klassa Carrier rocket super heavy class was the first super heavy launch vehicle being developed by the Russian space industry since the fall of the USSR The main developer is RSC Energia YeniseiFunctionOrbital Launch VehicleManufacturerRSC EnergiaCountry of originRussiaProject cost1 5 trln Roubles USD 20 8 billion SizeDiameter4 1 mMass3167 tonsStages2 Don 3 CapacityPayload to low Earth orbitMass103 140 metric tons 101 138 long tons Associated rocketsComparableFalcon Heavy Long March 9 Space Launch System SpaceX StarshipLaunch historyStatusDevelopment Postponed edit on Wikidata It is being developed within the framework of the federal target program Creation of a super heavy class space rocket complex for 2020 2030 1 and the program cost is estimated at 1 5 trillion roubles US 1 6 billion It is the main rocket of the Russian Lunar program The final design for the rocket was expected to be complete by autumn 2021 2 but the program appears to have been paused or stopped just before this expected completion date The first launch is expected to happen in 2028 from the Vostochny cosmodrome 3 Based on the Yenisei launch vehicle the Don launch vehicle RN STK 2 is being developed by adding another stage 4 It looks like this proposal has been at least paused 5 Anatoly ZakRussianSpaceWeb comRoadmap with two rockets on the right Yenisei and Don respectively Irtysh Soyuz 5 is a basis for the first stage Volga Soyuz 6 will be used as a basis for second stage Yenisei Yenisei cutaway Don Contents 1 Development 1 1 Chronology of development 2 Planned events 3 Design 3 1 Proposed variants 4 Flight tests 5 Applications 5 1 Lunar program payloads 5 2 Satellite constellation 6 See also 7 ReferencesDevelopment EditThe rocket got its name at the end of 2018 before that it was called RN STK super heavy launch vehicle Chronology of development Edit Event DateStart of work on the creation of the RD 171MV engine June 2017Start of research work on RD 0150 engine June 2017Preliminary estimate of the cost of R amp D on the RN STK October 2017Decree of the President of the Russian Federation on the creation of the RN STK January 2018Official name for RN STK January 2019Feasibility study of the RN STK project Spring 2019Draft design 2018 2019R amp D design and construction works 2020 2028Flight tests from 2028Planned events EditOctober 2021 end of technical design 2 needs update 2026 2028 construction and commissioning of infrastructure for a super heavy launch vehicle and a medium class rocket for launching crewed spacecraft from the Vostochny cosmodrome 6 Design EditThe first stage will consist of 6 blocks each block will be based on the first stage of the planned Irtysh Soyuz 5 rocket with an RD 171MV engine 7 Anatoly ZakRussianSpaceWeb com Roadmap with two rockets on the right Yenisei and Don respectively Irtysh Soyuz 5 is a basis for the first stage Volga Soyuz 6 will be used as a basis for second stage Yenisei Yenisei cutaway Don The second stage will consist of one block matching the first stage of Soyuz 6 with RD 180 as engine 7 The upper stage will be KVTK 7 Accelerating braking unit clarification needed Block DM 7 Proposed variants Edit Name of a rocket Yenisei 8 7 9 10 Don 8 10 Type Stage one Stage twoFirst launch 2028 2032 2035First stage 6xRD 171MV 6xRD 171MVSecond stage RD 180 RD 180Third stage 2 RD 0150Upper stage KVTK 2 RD 0146 KVTK 2 RD 0146Accelerating braking unit DM 11D58MF DM 11D58MFHeight max Launch weight t 3167 3281Thrust at ground level Thrust to weight ratioPayload LEO 200 km t 103 140Payload GTO 5500 km tPayload GEO 35 786 km t 26 29 5Payload to TLI 27 33Flight tests Edit Comparison of super heavy lift launch vehicles Masses listed are the maximum payload to low Earth orbit in metric tons Flight tests of a super heavy launch vehicle will take place in two stages from 2028 to 2035 11 The first stage of testing will take place in 2028 2032 It involves the launch of a crewed spacecraft a lunar take off and landing complex LVPK and other payloads on the trajectory of the flight around the Moon and circumlunar orbits in order to work out the elements of a crewed complex create a station in the orbit of the Moon and land on the lunar surface The second stage of testing will take place in 2032 2035 It is planned to launch LVPK and other uncrewed payloads for the construction and operation of a base on the lunar surface In addition this stage involves participation in international programs related to the study of Mars Applications EditThe super heavy rocket is supposed to be used in the Russian lunar program since the carrying capacity of the Angara A5V launch vehicle 37 5 tons to LEO is insufficient for these purposes Lunar program payloads Edit 20 ton Orel spacecraft 27 ton lunar landing and takeoff complex LPVK 32 ton lunar base module Satellite constellation Edit Spacecraft up to 30 tons to geostationary orbit Space telescopes 30 40 tons to the L2 Lagrange point in the Sun Earth systemSee also EditSpace Launch System Falcon Heavy Starship Long March 9References Edit Russia has developed the concept of the Federal Target Program for the creation of a super heavy rocket in Russian Ria Novosti 28 May 2019 a b The design of the Russian super heavy rocket will be completed in 2021 In Russian Izvestia 23 August 2020 Roskosmos has named the timing of the launch of a super heavy rocket in Russian Ria Novosti 17 July 2018 Possible dates for the launch of the Don super heavy rocket have been named in Russian Ria Novosti 14 February 2019 Better late than never why the development of the Yenisei launch vehicle was stopped 17 September 2021 Russian super heavy rocket will be able to launch at least 70 tons of cargo into orbit In Russian TASS 14 July 2017 a b c d e New generation locomotives in Russian Russkiy Kosmos 15 34 39 2020 a b Roscosmos unveils characteristics of super heavy rockets for flights to the Moon In Russian Ria Novosti 24 April 2019 The Yenisei super heavy rocket RussianSpaceWeb a b Transformation of Roscosmos Russki Kosmos 7 2 7 July 2019 RSC Energia flight tests of the Soyuz 5 rocket will take place from 2022 to 2025 In Russian TASS 3 July 2018 Retrieved from https en wikipedia org w index php title Yenisei rocket amp oldid 1123712766, wikipedia, wiki, book, books, library,
