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- Dragon_(rocket) abstract "The Dragon is a two-stage French solid propellant sounding rocket used for high altitude research. Its first stage was a Stromboli engine (diameter 56 cm) which burned 675 kg of fuel in 16 s and so produced a maximum thrust of 88 kN. A Belier engine was used as the upper stage. It belonged thereby to a family of solid-propellant rockets derived from the Belier, including the Centaure, the Dauphin and the Eridan. A payload of 30 to 120 kg could be carried on parabolic with apogees between 440 km (270 mi) (Dragon 2B) and 4560 km (340 mi)(Dragon III) The Dragon was built in several versions including the Dragon-2B, and Dragon-3, Dragons have been launched from Andøya, Norway; Biscarrosse, France; Dumont d'Urville, Antartica; Chamical, Argentina; Hammaguir, Algeria; Kerguelen Islands; Kourou, French Guiana; Mar Chiquita, Argentina; Salto di Quirra, Sardinia; Sonmiani, Pakistan; Thumba, India; and Vík í Mýrdal, Iceland.".
- Dragon_(rocket) wikiPageID "1435196".
- Dragon_(rocket) wikiPageLength "2656".
- Dragon_(rocket) wikiPageOutDegree "21".
- Dragon_(rocket) wikiPageRevisionID "675810673".
- Dragon_(rocket) wikiPageWikiLink Andøya_Space_Center.
- Dragon_(rocket) wikiPageWikiLink Belier.
- Dragon_(rocket) wikiPageWikiLink CELPA_(El_Chamical).
- Dragon_(rocket) wikiPageWikiLink CELPA_(Mar_Chiquita).
- Dragon_(rocket) wikiPageWikiLink Category:Sounding_rockets_of_France.
- Dragon_(rocket) wikiPageWikiLink Centaure.
- Dragon_(rocket) wikiPageWikiLink DGA_Essais_de_missiles.
- Dragon_(rocket) wikiPageWikiLink Dauphin_(rocket).
- Dragon_(rocket) wikiPageWikiLink Dumont_dUrville_Station.
- Dragon_(rocket) wikiPageWikiLink Eridan.
- Dragon_(rocket) wikiPageWikiLink France.
- Dragon_(rocket) wikiPageWikiLink Guiana_Space_Centre.
- Dragon_(rocket) wikiPageWikiLink Hammaguir.
- Dragon_(rocket) wikiPageWikiLink Kerguelen_Islands.
- Dragon_(rocket) wikiPageWikiLink Multistage_rocket.
- Dragon_(rocket) wikiPageWikiLink Propellant.
- Dragon_(rocket) wikiPageWikiLink Salto_di_Quirra.
- Dragon_(rocket) wikiPageWikiLink Sonmiani_(space_facility).
- Dragon_(rocket) wikiPageWikiLink Sounding_rocket.
- Dragon_(rocket) wikiPageWikiLink Thumba_Equatorial_Rocket_Launching_Station.
- Dragon_(rocket) wikiPageWikiLink Vík_í_Mýrdal.
- Dragon_(rocket) wikiPageWikiLinkText "Dragon (rocket)".
- Dragon_(rocket) wikiPageWikiLinkText "Dragon I".
- Dragon_(rocket) wikiPageWikiLinkText "Dragon rockets".
- Dragon_(rocket) wikiPageWikiLinkText "Dragon".
- Dragon_(rocket) wikiPageUsesTemplate Template:About.
- Dragon_(rocket) wikiPageUsesTemplate Template:Not_in_citation.
- Dragon_(rocket) wikiPageUsesTemplate Template:Reflist.
- Dragon_(rocket) wikiPageUsesTemplate Template:Rocket-stub.
- Dragon_(rocket) subject Category:Sounding_rockets_of_France.
- Dragon_(rocket) hypernym Propellant.
- Dragon_(rocket) type ChemicalCompound.
- Dragon_(rocket) type Vehicle.
- Dragon_(rocket) comment "The Dragon is a two-stage French solid propellant sounding rocket used for high altitude research. Its first stage was a Stromboli engine (diameter 56 cm) which burned 675 kg of fuel in 16 s and so produced a maximum thrust of 88 kN. A Belier engine was used as the upper stage. It belonged thereby to a family of solid-propellant rockets derived from the Belier, including the Centaure, the Dauphin and the Eridan.".
- Dragon_(rocket) label "Dragon (rocket)".
- Dragon_(rocket) sameAs Q540734.
- Dragon_(rocket) sameAs Dragon_(Rakete).
- Dragon_(rocket) sameAs Dragon_(cohete).
- Dragon_(rocket) sameAs ドラゴン_(ロケット).
- Dragon_(rocket) sameAs Dragon_(foguete).
- Dragon_(rocket) sameAs m.05190n.
- Dragon_(rocket) sameAs Q540734.
- Dragon_(rocket) wasDerivedFrom Dragon_(rocket)?oldid=675810673.
- Dragon_(rocket) isPrimaryTopicOf Dragon_(rocket).