File:Viking 5C Rocketengine.jpg
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.
![]() |
Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, 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 license is included in the section entitled GNU Free Documentation License. |
Click on a date/time to view the file as it appeared at that time.
Date/Time | Thumbnail | Dimensions | User | Comment | |
---|---|---|---|---|---|
current | 07:44, 29 June 2008 | ![]() | 2,336 × 3,504 (3.66 MB) | 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 |
The following other wikis use this file: