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.
လိက်တအ်ဂှ် သၠးကဵုလဝ် အခေါင် သွက်ဂွံ စၠောအ်ကပ်ပဳ၊ ပရး ကီု သီုကဵု ပလေဝ်ပခိုဟ်ပတိုန် အတိုင်သၞောတ်ဝ် GNU Free Documentation License, တုဲ မူ ၁.၂ ဟွံသေင်မ္ဂး မူတြေံနူဂှ် မတြးပတိတ် နကဵု သၞောတ်ဝ်လာင်ဇြေန် 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.http://www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue
{{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