Technical Data
| Version | Viking 2B | Viking 4 | Viking 4B | Viking 5C | Viking 6 | |
|---|---|---|---|---|---|---|
| Height | 2.87 m | 2.87 m | 3.51 m | 3.51 m | 2.87 m | 2.87 m |
| Diameter | 0.99 m | 0.99 m | 1.70 m | 1.70 m | 0.99 m | 0.99 m |
| Mass | ? | ? | 826 kg | 826 kg | 826 kg | 826 kg |
| Fuels | Dinitrogen tetroxide and UDMH in Ratio 1.86:1 | Dinitrogen tetroxide and UH 25 in Ratio 1.70:1 | Dinitrogen tetroxide and UDMH in Ratio 1.86:1 | Dinitrogen tetroxide and UH 25 in Ratio 1.70:1 | Dinitrogen tetroxide and UH 25 in Ratio 1.70:1 | Dinitrogen tetroxide and UH 25 in Ratio 1.71:1 |
| Fuel Consumption | ca. 275 kg/s | ca. 275 kg/s | ca. 275 kg/s | ca. 275 kg/s | ca. 275 kg/s | ca. 275 kg/s |
| Performance of the turbine | 2500 kW/10,000 U/min. | 2500 kW/10,000 U/min. | 2500 kW/10,000 U/min. | 2500 kW/10,000 U/min. | 2500 kW/10,000 U/min. | 2500 kW/10,000 U/min. |
| Vacuum thrust | 690 kN | ? | 713 kN | 800 kN | 758 kN | 750 kN |
| SeaLevel thrust | 611 kN | 643 kN | - | - | 678 kN | ? |
| Use | Ariane 1, | Ariane 2, 3 | Ariane 1 | Ariane 2 - 4 | Ariane 4 | PAL (Ariane 4 liquid booster ) |
Read more about this topic: Viking (rocket Engine)
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