File:Viking 5C rocketengine.jpg

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Captions

Captions

Viking 5C Rocket Engine

Summary

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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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current07:44, 29 June 2008Thumbnail for version as of 07:44, 29 June 20082,336 × 3,504 (3.66 MB)Sanjay ach (talk | contribs){{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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