RD-107 topic
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| Status |
| Used in rocket stages |
| Government designation |
- 8D74
| Manufactured by |
| Designed by |
| Design period |
|
start
|
end
|
|---|---|
|
|
| Use period |
|
start
|
|---|
|
| Diameter |
- 1.85m
| Height |
- 2.865m
| Thrust (vacuum) |
- 999,600.0N
| Thrust (sea level) |
- 813,400.0N
| Isp (vacuum) |
- 313.0s
| Isp (sea level) |
- 256.0s
| Dry mass |
- 1,190.0kg
| Throttle ratio |
| Wet mass |
- 1,300.0kg
| Engine cycle |
| Fuel |
| Oxidizer |
| Oxidizer/fuel ratio |
- 2.47
| Expansion ratio |
| Chamber pressure |
- 59.0bar
| Number of chambers |
- 4
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