ドラゴン (ロケット)
1. Dragon (rocket)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.
Read “Dragon (rocket)” on English Wikipedia
Read “ドラゴン (ロケット)” on Japanese Wikipedia
Read “Dragon (rocket)” on DBpedia
Read “Dragon (rocket)” on English Wikipedia
Read “ドラゴン (ロケット)” on Japanese Wikipedia
Read “Dragon (rocket)” on DBpedia
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