Difference between revisions of "Sojus (rocket)"
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|diameter=10.3 metres | |diameter=10.3 metres | ||
|height=45.6 metres | |height=45.6 metres | ||
| − | |weight= | + | |weight= 308,000 kilograms |
|engine_power= | |engine_power= | ||
|specific_impulse= | |specific_impulse= | ||
Latest revision as of 11:11, 15 April 2018
| This page is a work in progress by its author(s) and should not be considered final. |
| Sojus Rocket | |
|---|---|
 Sojus 83 launching | |
| Type | Rocket |
| Place of origin | Cerdani Democratic Republic |
| Service history | |
| In service | 1965-present |
| Used by | DDR Raumfahrtprogramm |
| Production history | |
| Manufacturer | Cerdani Space Program |
| Specifications | |
| Weight | 308,000 kilograms |
| Height | 45.6 metres |
| Diameter | 10.3 metres |
