バイキングエンジン
1. Viking (rocket engine)The Viking rocket engines were members of a series of bipropellant engines for the first and second stages of the Ariane 1 through Ariane 4 commercial launch vehicles, using storable, hypergolic propellants, N2O4/UH 25 The earliest versions, developed in 1973, had a thrust of about 390 kN. The version used on the Ariane 4 first stage, which clustered four together, had 667 kN thrust each. The second stage of Ariane used a single Viking.
Read “Viking (rocket engine)” on English Wikipedia
Read “バイキングエンジン” on Japanese Wikipedia
Read “Viking (rocket engine)” on DBpedia
Read “Viking (rocket engine)” on English Wikipedia
Read “バイキングエンジン” on Japanese Wikipedia
Read “Viking (rocket engine)” on DBpedia
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