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- Universal_Rocket_Module abstract "Universal Rocket Module (URM) is the name of the modular liquid fuelled first and second stage of the Angara expendable launch system. The first stage and booster variant is referred to as URM-1, while the second stage is referred to as URM-2. The URM-2 is derived from the Soyuz-2 Block I second stage.URM-1 is a unitary structure 2.9 meters in diameter and 25 meters in length that includes an oxidizer tank, a fuel tank (both tanks being coupled by a spacer) and an RD-191 engine burning RP-1 fuel with liquid oxygen producing a thrust of 1.92 MN. URM-1 was first flown in 2014 on the Angara 1.2PP suborbital test flight. Angara can fly with either one URM-1 in the case of Angara 1.2 and Angara 1.2PP, or one URM-1 as a sustainer core with four additional URM-1s as boosters for Angara A5.URM-2 is a modified Block I stage, 3.6 meters in diameter and 6.9 meters in length. It is powered by a single RD-0124A producing 294 kilonewtons, derived from Block I's RD-0124. URM-2 was first flight tested on Angara 1.2PP, but will fly in operation only on the Angara A5. The operational Angara 1.2 will also use a modified Block I powered by the RD-0124A as a second stage, though this stage will have a diameter of no more than 2.9 meters.The Naro-1 launch vehicle was based on the URM-1 with a reduced thrust RD-191, called RD-151, combined with a solid-fueled second stage built by Republic of Korea KARI.".
- Universal_Rocket_Module wikiPageExternalLink main.php?id=44.
- Universal_Rocket_Module wikiPageExternalLink angara.html.
- Universal_Rocket_Module wikiPageID "24040839".
- Universal_Rocket_Module wikiPageLength "3689".
- Universal_Rocket_Module wikiPageOutDegree "32".
- Universal_Rocket_Module wikiPageRevisionID "672097871".
- Universal_Rocket_Module wikiPageWikiLink Angara-1.2pp.
- Universal_Rocket_Module wikiPageWikiLink Angara_(rocket_family).
- Universal_Rocket_Module wikiPageWikiLink Atlas_V.
- Universal_Rocket_Module wikiPageWikiLink Category:Rocketry.
- Universal_Rocket_Module wikiPageWikiLink Category:Spacecraft_components.
- Universal_Rocket_Module wikiPageWikiLink Common_Booster_Core.
- Universal_Rocket_Module wikiPageWikiLink Common_Core_Booster.
- Universal_Rocket_Module wikiPageWikiLink Delta_IV.
- Universal_Rocket_Module wikiPageWikiLink Expendable_launch_system.
- Universal_Rocket_Module wikiPageWikiLink Kerosene.
- Universal_Rocket_Module wikiPageWikiLink Khrunichev_State_Research_and_Production_Space_Center.
- Universal_Rocket_Module wikiPageWikiLink Korea_Aerospace_Research_Institute.
- Universal_Rocket_Module wikiPageWikiLink Launch_vehicle.
- Universal_Rocket_Module wikiPageWikiLink Liquid-propellant_rocket.
- Universal_Rocket_Module wikiPageWikiLink Liquid_oxygen.
- Universal_Rocket_Module wikiPageWikiLink Liquid_rocket_booster.
- Universal_Rocket_Module wikiPageWikiLink Naro-1.
- Universal_Rocket_Module wikiPageWikiLink Newton_(unit).
- Universal_Rocket_Module wikiPageWikiLink RD-0124.
- Universal_Rocket_Module wikiPageWikiLink RD-191.
- Universal_Rocket_Module wikiPageWikiLink RP-1.
- Universal_Rocket_Module wikiPageWikiLink South_Korea.
- Universal_Rocket_Module wikiPageWikiLink Soyuz-2_(rocket).
- Universal_Rocket_Module wikiPageWikiLinkText "URM-1".
- Universal_Rocket_Module wikiPageWikiLinkText "URM-2".
- Universal_Rocket_Module wikiPageWikiLinkText "Universal Rocket Module".
- Universal_Rocket_Module wikiPageWikiLinkText "universal rocket module".
- Universal_Rocket_Module country "Russia".
- Universal_Rocket_Module engines "1".
- Universal_Rocket_Module fuel Kerosene.
- Universal_Rocket_Module fuel Liquid_oxygen.
- Universal_Rocket_Module manufacturer Khrunichev_State_Research_and_Production_Space_Center.
- Universal_Rocket_Module name "URM-1".
- Universal_Rocket_Module name "URM-2".
- Universal_Rocket_Module rockets "Angara A5 stage 2".
- Universal_Rocket_Module rockets "Angara stage 1 and boosters".
- Universal_Rocket_Module si "311.0".
- Universal_Rocket_Module si "359.0".
- Universal_Rocket_Module time "214.0".
- Universal_Rocket_Module time "325.0".
- Universal_Rocket_Module time "424.0".
- Universal_Rocket_Module wikiPageUsesTemplate Template:Convert.
- Universal_Rocket_Module wikiPageUsesTemplate Template:Infobox_rocket_stage.
- Universal_Rocket_Module wikiPageUsesTemplate Template:Reflist.
- Universal_Rocket_Module wikiPageUsesTemplate Template:Rocketry-stub.
- Universal_Rocket_Module subject Category:Rocketry.
- Universal_Rocket_Module subject Category:Spacecraft_components.
- Universal_Rocket_Module hypernym Stage.
- Universal_Rocket_Module type Person.
- Universal_Rocket_Module type Ballistic.
- Universal_Rocket_Module type Component.
- Universal_Rocket_Module type Technology.
- Universal_Rocket_Module comment "Universal Rocket Module (URM) is the name of the modular liquid fuelled first and second stage of the Angara expendable launch system. The first stage and booster variant is referred to as URM-1, while the second stage is referred to as URM-2.".
- Universal_Rocket_Module label "Universal Rocket Module".
- Universal_Rocket_Module sameAs Q7894056.
- Universal_Rocket_Module sameAs ユニバーサル・ロケット・モジュール.
- Universal_Rocket_Module sameAs m.080k8j5.
- Universal_Rocket_Module sameAs Универсальный_ракетный_модуль.
- Universal_Rocket_Module sameAs Q7894056.
- Universal_Rocket_Module wasDerivedFrom Universal_Rocket_Module?oldid=672097871.
- Universal_Rocket_Module isPrimaryTopicOf Universal_Rocket_Module.