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Stock Photo: Viking Rocket Engine

ID 307205731 © Faazawanz | Megapixl.com

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: dinitrogen tetroxide and UH 25, a mixture of 75% UDMH and 25% hydrazine[3] (originally UDMH).

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Viking Rocket Engine

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