warhammerautist
kiwifarms.net
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- 1 de Mayo, 2024
Thread that highlights any of their technological breakthroughs for space, what projects they are doing, who they are competing against and what they are doing with any partner countries involved.
Angara Rocket Projects
Angara-A5M: https://ria.ru/20240423/varochko-1941549788.html?ysclid=lxwk4ag283375449809 https://ria.ru/20240417/angara-1940631086.html?in=t test launch will be in 2027, payload to LEO is 27 tons, RD-191M engine has 10% more thrust increasing the past payload of the old A5 rocket.
Angara-A5V: https://tass.com/science/866601 In 2016 they predicted it would launch in 2026, https://ria.ru/20240417/kosmos-1940631819.html?in=t predict that flight tests will be in 2030. 1st and 2nd stage engines are returnable, 3rd stage will be hydrogen with a payload of 38 tons to orbit.
Amur Rocket Project
https://rg.ru/2020/10/05/pusk-mnogo...n-na-2026-god.html?ysclid=lxwo5onxpw931403132 launch was scheduled for 2026. https://www.interfax.ru/russia/955516 2024 source states launch is scheduled for 2030. Picture is self explanatory, supposedly 50-100 re-use claims according different sources out there. One even claims 300 re-uses https://web.archive.org/web/20201011064350/https://www.roscosmos.ru/29357/
Miniature/Winged Body Rocket Projects.
Current re-usable rocket methods to what Space X and what they are trying to do with Amur is having half the fuel burn to reach orbit and half the fuel to burn to land and be re-used. A more cheaper method for re-usability is using control surfaces of using wings with some fuel to re-land. Sadly the Baikal rocket went nowhere but they are going back to winged body designs for re-usability which is something not worth underestimating because of market potential.
Krylo-SV/Irkut?: stages of rocket re-usability.
I think the Krylo-SV and Irkut are the same fucking rocket with two different name. https://vpk.name/en/552112_the-timi...winged-stage-krylo-sv-has-been-announced.html https://en.topwar.ru/188073-russkij...eta-nositel-navjazat-konkurenciju-zapadu.html uses methane for launch and a turbo jet engine with wings and parachute to land and re-use engine. One time use is 580 kilograms for LEO re-usable is 400 kilograms to LEO, test flight is supposedly scheduled some time this year.
Start-1M: https://tass.com/science/1774381 ultra-light single use rocket ready for flight in 2026. No further details about it other than that.
https://rostec.ru/news/rostekh-sozd...ateli-dlya-sverkhlegkikh-kosmicheskikh-raket/ UEC is creating engines that will launch 250kg to orbit. Maybe they are working on a different light rocket design and investment for this project is 2.7 billion rubles.
Yenisei/Don Rocket
super heavy rocket designs, the Yenisei was for 103 tons to orbit and the Don rocket was 140 tons to orbit. Yenisei was expected to fly in 2028 by design was cancelled awhile back supposedly for a methane design over a kerosene design. https://tass.ru/kosmos/20526431 Turns out the new super heavy class rocket is supposedly scheduled for a 2033 flight with the investment in the project at 600 billion rubles, payload is 90 tons to LEO.
Nuklon Nuclear Space Tug
Zeus is to be launched in 2030 being a nuclear reactor with MPD thrusters dropping off multiple payloads in its travels in the solar system at a 50 month time period.
ROSS(Russian Orbital Space Station
expected to be completed by 2035
Technological Breakthroughs
News that is considered of high importance to make major changes in space travel.
Fuel Replacement for Xenon: https://www.gazeta.ru/science/news/2022/08/17/18345194.shtml?ysclid=l7119e38n3971661861 https://glav.su/forum/threads/1668028 Xenon is super expensive do Krypton and Argon are being considered solutions for MPD thrusters for high speed space travel.
Aerospike Engines: https://tass.ru/kosmos/18947311?ysclid=lxwubh4lo6104991468
Material that burns above 4000 Celsius from kinetic heat: https://russian.rt.com/science/article/748188-karbonitrid-gafniya
3000 second engine thrust new record: https://nurman.ru/news/jarlburensta...y-dlitelnostyu-raboty-r16444/#google_vignette
Angara Rocket Projects
Angara-A5M: https://ria.ru/20240423/varochko-1941549788.html?ysclid=lxwk4ag283375449809 https://ria.ru/20240417/angara-1940631086.html?in=t test launch will be in 2027, payload to LEO is 27 tons, RD-191M engine has 10% more thrust increasing the past payload of the old A5 rocket.
Angara-A5V: https://tass.com/science/866601 In 2016 they predicted it would launch in 2026, https://ria.ru/20240417/kosmos-1940631819.html?in=t predict that flight tests will be in 2030. 1st and 2nd stage engines are returnable, 3rd stage will be hydrogen with a payload of 38 tons to orbit.
Amur Rocket Project
https://rg.ru/2020/10/05/pusk-mnogo...n-na-2026-god.html?ysclid=lxwo5onxpw931403132 launch was scheduled for 2026. https://www.interfax.ru/russia/955516 2024 source states launch is scheduled for 2030. Picture is self explanatory, supposedly 50-100 re-use claims according different sources out there. One even claims 300 re-uses https://web.archive.org/web/20201011064350/https://www.roscosmos.ru/29357/
Miniature/Winged Body Rocket Projects.
Current re-usable rocket methods to what Space X and what they are trying to do with Amur is having half the fuel burn to reach orbit and half the fuel to burn to land and be re-used. A more cheaper method for re-usability is using control surfaces of using wings with some fuel to re-land. Sadly the Baikal rocket went nowhere but they are going back to winged body designs for re-usability which is something not worth underestimating because of market potential.
Krylo-SV/Irkut?: stages of rocket re-usability.
I think the Krylo-SV and Irkut are the same fucking rocket with two different name. https://vpk.name/en/552112_the-timi...winged-stage-krylo-sv-has-been-announced.html https://en.topwar.ru/188073-russkij...eta-nositel-navjazat-konkurenciju-zapadu.html uses methane for launch and a turbo jet engine with wings and parachute to land and re-use engine. One time use is 580 kilograms for LEO re-usable is 400 kilograms to LEO, test flight is supposedly scheduled some time this year.
Start-1M: https://tass.com/science/1774381 ultra-light single use rocket ready for flight in 2026. No further details about it other than that.
https://rostec.ru/news/rostekh-sozd...ateli-dlya-sverkhlegkikh-kosmicheskikh-raket/ UEC is creating engines that will launch 250kg to orbit. Maybe they are working on a different light rocket design and investment for this project is 2.7 billion rubles.
Yenisei/Don Rocket
super heavy rocket designs, the Yenisei was for 103 tons to orbit and the Don rocket was 140 tons to orbit. Yenisei was expected to fly in 2028 by design was cancelled awhile back supposedly for a methane design over a kerosene design. https://tass.ru/kosmos/20526431 Turns out the new super heavy class rocket is supposedly scheduled for a 2033 flight with the investment in the project at 600 billion rubles, payload is 90 tons to LEO.
Nuklon Nuclear Space Tug
Zeus is to be launched in 2030 being a nuclear reactor with MPD thrusters dropping off multiple payloads in its travels in the solar system at a 50 month time period.
ROSS(Russian Orbital Space Station
expected to be completed by 2035
Technological Breakthroughs
News that is considered of high importance to make major changes in space travel.
Fuel Replacement for Xenon: https://www.gazeta.ru/science/news/2022/08/17/18345194.shtml?ysclid=l7119e38n3971661861 https://glav.su/forum/threads/1668028 Xenon is super expensive do Krypton and Argon are being considered solutions for MPD thrusters for high speed space travel.
Aerospike Engines: https://tass.ru/kosmos/18947311?ysclid=lxwubh4lo6104991468
Material that burns above 4000 Celsius from kinetic heat: https://russian.rt.com/science/article/748188-karbonitrid-gafniya
3000 second engine thrust new record: https://nurman.ru/news/jarlburensta...y-dlitelnostyu-raboty-r16444/#google_vignette