Viking
From Spacefaring
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.
Haupttriebwerk einer Ariane 4, Viking 5c (15590922892)| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Haupttriebwerk einer Ariane 4, Viking 5c (15590922892) | Commons | ||
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