File:Viking 5C rocketengine.jpg
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Summary
| Description |
English: The Viking 5C Rocket Engine. The engine was designed and manufactured by six countries: France, Germany, Spain, Belgium, Sweden and Italy. It was used in first stage of Ariane 4 from 1990 to 2003. Picture taken at the National Air and Space Museum's Steven F. Udvar-Hazy Center, Chantilly, Virginia, USA.
Length: 2.87 m (9 ft 5 in). Weight: 399 Kg (880 lb). Thrust: 760700 N (171500 lb) Propellants: Nitrogen tetroxide & unsymmetrical dimethyl hydrazine (UDMH). Manufacturer: SNECMA for the European Space Agency. |
| Date | |
| Source | Own work |
| Author | Sanjay Acharya |
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Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation Licence, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the licence is included in the section entitled GNU Free Documentation Licence. |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 13:14, 29 June 2008 | | 2,336 × 3,504 (3.66 MB) | wikimediacommons>Sanjay ach | {{Information |Description={{en|1=The Viking 5C Rocket Engine. The engine was designed and manufactured by six countries: France, Germany, Spain, Belgium, Sweden and Italy. It was used in first stage of Ariane 4 from 1990 to 2003. Length: 2.87 m (9 ft 5 |
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