ꯐꯥꯏꯜ:Viking 5C rocketengine.jpg
ꯃꯁꯤꯒꯤ ꯄ꯭ꯔꯚꯤꯌꯨ ꯑꯁꯤꯒꯤ ꯁꯥꯏꯓ: ২২০ × ৩৩০ ꯄꯤꯛꯆꯦꯜꯁ. ꯑꯇꯩ ꯁꯦꯡꯅ ꯌꯦꯡꯕ ꯌꯥꯕ: ১৬০ × ২৪০ ꯄꯤꯛꯆꯦꯜꯁ | ২,৩৩৬ × ৩,৫০৪ ꯄꯤꯛꯆꯦꯜꯁ.
ꯐꯥꯏꯜ ꯑꯁꯦꯡꯕ (২,৩৩৬ × ৩,৫০৪ ꯄꯤꯛꯆꯦꯜꯁ, ꯐꯥꯏꯜ ꯆꯥꯎꯕꯒꯤ ꯆꯥꯡ: ৩.৬৬ MB, MIME ꯃꯈꯜ: image/jpeg)
ꯑꯇꯦꯟꯕꯥ ꯁꯟꯗꯣꯛꯅꯥ ꯇꯥꯛꯄꯥ
| ꯁꯟꯗꯣꯛꯅꯥ ꯇꯥꯛꯄꯥViking 5C rocketengine.jpg |
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. |
| ꯆꯩꯆꯠ | |
| ꯍꯧꯔꯛꯐꯛ | ꯏꯁꯥ ꯏꯊꯟꯇꯒꯤ ꯑꯣꯏꯕꯥ ꯊꯕꯛ |
| ꯄꯨꯊꯣꯛꯂꯤꯕ ꯃꯤ | Sanjay Acharya |
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Viking 5C Rocket Engine
ꯐꯥꯏꯜꯒꯤ ꯄꯨꯋꯥꯔꯤ
ꯆꯩꯆꯠ/ꯃꯇꯝꯗ ꯅꯝꯃꯨ ꯃꯇꯝ ꯑꯗꯨꯗ ꯐꯥꯏꯜ ꯑꯗꯨ ꯎꯅꯕ
| ꯆꯩꯆꯠ/ꯃꯇꯝ | ꯈꯨꯠꯄꯤꯈꯨꯖꯤꯟ | ꯄꯥꯛ ꯆꯥꯎꯕꯥ | ꯁꯤꯖꯤꯟꯅꯔꯤꯕ | ꯑꯄꯥꯝꯕ ꯐꯣꯡꯗꯣꯛ ꯎ | |
|---|---|---|---|---|---|
| ꯍꯧꯖꯤꯛꯀꯤ | ꯱꯳:꯱꯴, ꯲꯹ ꯖꯨꯟ ꯲꯰꯰꯸ |  | ২,৩৩৬ × ৩,৫০৪ (৩.৬৬ MB) | smartcommons>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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