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Dragon (rocket)
The Dragon is a two-stage French solid propellant sounding rocket used for high altitude research.〔(【引用サイトリンク】title=Dragon 1 )〕 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)〔(【引用サイトリンク】title=Dragon 2B )〕 and 4560 km (340 mi)(Dragon III)〔(【引用サイトリンク】title=Dragon 3 )〕 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.〔(【引用サイトリンク】title=Overview of rocket launch sites worldwide )〕
==References==
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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