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- RD-0410 abstract "RD-0410 (РД-0410, GRAU index: 11B91) was a Soviet nuclear thermal rocket engine developed from 1965 through the 1980s using liquid hydrogen propellant. The engine was ground-tested at the Semipalatinsk Test Site, and its use was incorporated in the Kurchatov Mars 1994 manned mission proposal.This engine had slightly higher performance (exhaust temperature and specific impulse) over NERVA (the U.S. nuclear thermal rocket engine project), but much less thrust: only 35.2 kN compared to 333.6 kN of NERVA. The design of the reactor core included thermal insulation between uranium carbide/tungsten carbide fuel and the zirconium hydride moderator. This solution allowed for a very compact reactor core design. Hydrogen flow cooled the moderator first allowing to keep very low neutron energy and high fission cross-section, then it was heated by the direct contact to the fuel rods. To prevent the chemical reaction between carbide and hydrogen, about 1 pct of heptane was added to the hydrogen after the moderator passage.The hydrogen boost turbopump was designed by KBKhA in Voronezh.".
- RD-0410 wikiPageExternalLink 58.shtml.
- RD-0410 wikiPageExternalLink sovermal.htm.
- RD-0410 wikiPageExternalLink 1141-k-marsu-na-reaktore.
- RD-0410 wikiPageExternalLink watch?v=nvZjmj1bopw.
- RD-0410 wikiPageID "20615010".
- RD-0410 wikiPageLength "3021".
- RD-0410 wikiPageOutDegree "14".
- RD-0410 wikiPageRevisionID "681848065".
- RD-0410 wikiPageWikiLink Category:Nuclear_spacecraft_propulsion.
- RD-0410 wikiPageWikiLink Chemical_Automatics_Design_Bureau.
- RD-0410 wikiPageWikiLink GRAU.
- RD-0410 wikiPageWikiLink GRAU_index.
- RD-0410 wikiPageWikiLink Heptane.
- RD-0410 wikiPageWikiLink KBKhA.
- RD-0410 wikiPageWikiLink Liquid_hydrogen.
- RD-0410 wikiPageWikiLink List_of_manned_Mars_mission_plans_in_the_20th_century.
- RD-0410 wikiPageWikiLink NERVA.
- RD-0410 wikiPageWikiLink Nuclear_Thermal_Rocket.
- RD-0410 wikiPageWikiLink Nuclear_thermal_rocket.
- RD-0410 wikiPageWikiLink Semipalatinsk_Test_Site.
- RD-0410 wikiPageWikiLink Uranium_carbide.
- RD-0410 wikiPageWikiLink Voronezh.
- RD-0410 wikiPageWikiLink Zirconium_hydride.
- RD-0410 wikiPageWikiLinkText "11B91 (RD0410)".
- RD-0410 wikiPageWikiLinkText "RD-0410".
- RD-0410 hasPhotoCollection RD-0410.
- RD-0410 wikiPageUsesTemplate Template:Reflist.
- RD-0410 wikiPageUsesTemplate Template:Rocket-stub.
- RD-0410 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-0410 subject Category:Nuclear_spacecraft_propulsion.
- RD-0410 hypernym Engine.
- RD-0410 type Article.
- RD-0410 type Software.
- RD-0410 type Article.
- RD-0410 comment "RD-0410 (РД-0410, GRAU index: 11B91) was a Soviet nuclear thermal rocket engine developed from 1965 through the 1980s using liquid hydrogen propellant. The engine was ground-tested at the Semipalatinsk Test Site, and its use was incorporated in the Kurchatov Mars 1994 manned mission proposal.This engine had slightly higher performance (exhaust temperature and specific impulse) over NERVA (the U.S.".
- RD-0410 label "RD-0410".
- RD-0410 sameAs m.0523nd9.
- RD-0410 sameAs РД-0410.
- RD-0410 sameAs Q4386493.
- RD-0410 sameAs Q4386493.
- RD-0410 wasDerivedFrom RD-0410?oldid=681848065.
- RD-0410 isPrimaryTopicOf RD-0410.