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- UH_25 abstract "UH 25 is a fuel mixture for rockets. It was developed for the European Ariane 2-4 launch vehicles.UH 25 was developed after a disaster during flight 2 of the Ariane 1 rocket. During launch, one of the four Viking engines on the first stage developed a combustion instability which led to an engine fire, subsequent explosion and destruction of the vehicle. Following this event and starting with Ariane 2, the fuel was changed from pure UDMH to the mixture UH 25.UH 25 was used in Ariane rocket versions 2 through 4, and in the Indian GSLV Mk IIIUH 25 is a mixture of 75% UDMH and 25% hydrazine hydrate. It is hypergolic with dinitrogen tetroxide as oxidizer, and both can be stored as liquids at room temperature.".
- UH_25 thumbnail Hazard_T.svg?width=300.
- UH_25 wikiPageExternalLink index.php?title=UH_25&action=history.
- UH_25 wikiPageID "4016564".
- UH_25 wikiPageLength "2210".
- UH_25 wikiPageOutDegree "14".
- UH_25 wikiPageRevisionID "660078154".
- UH_25 wikiPageWikiLink Aerozine_50.
- UH_25 wikiPageWikiLink Ariane_(rocket_family).
- UH_25 wikiPageWikiLink C-Stoff.
- UH_25 wikiPageWikiLink Category:Rocket_fuels.
- UH_25 wikiPageWikiLink Dinitrogen_tetroxide.
- UH_25 wikiPageWikiLink GNU_Free_Documentation_License.
- UH_25 wikiPageWikiLink Geosynchronous_Satellite_Launch_Vehicle_Mk_III.
- UH_25 wikiPageWikiLink Hydrazine.
- UH_25 wikiPageWikiLink Hypergolic_propellant.
- UH_25 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- UH_25 wikiPageWikiLink Viking_(rocket_engine).
- UH_25 wikiPageWikiLink Walter_HWK_109-509.
- UH_25 wikiPageWikiLink File:Hazard_F.svg.
- UH_25 wikiPageWikiLink File:Hazard_T.svg.
- UH_25 wikiPageWikiLinkText "UH 25".
- UH_25 wikiPageWikiLinkText "UH25".
- UH_25 wikiPageUsesTemplate Template:Reflist.
- UH_25 wikiPageUsesTemplate Template:Rocket-stub.
- UH_25 subject Category:Rocket_fuels.
- UH_25 hypernym Mixture.
- UH_25 type ChemicalSubstance.
- UH_25 type Fuel.
- UH_25 type Propellant.
- UH_25 comment "UH 25 is a fuel mixture for rockets. It was developed for the European Ariane 2-4 launch vehicles.UH 25 was developed after a disaster during flight 2 of the Ariane 1 rocket. During launch, one of the four Viking engines on the first stage developed a combustion instability which led to an engine fire, subsequent explosion and destruction of the vehicle.".
- UH_25 label "UH 25".
- UH_25 sameAs Q467819.
- UH_25 sameAs UH_25.
- UH_25 sameAs UH_25.
- UH_25 sameAs UH_25.
- UH_25 sameAs UH_25.
- UH_25 sameAs m.0bcpmx.
- UH_25 sameAs Q467819.
- UH_25 wasDerivedFrom UH_25?oldid=660078154.
- UH_25 depiction Hazard_T.svg.
- UH_25 isPrimaryTopicOf UH_25.