RD-0108
| Kraj pochodzenia | |
|---|---|
| Projektant | |
| Wykorzystanie | |
| Materiały napędowe | |
| Pierwszy lot |
1960 |
| Ostatni lot |
1976 |
| Osiągi | |
| Siła ciągu w próżni |
279,9 kN |
| Impuls właściwy w próżni |
326 s |
| Maks. czas działania |
250 s |
| Parametry | |
| Komory spalania |
4 |
| Ciśnienie w komorze |
68,2 bar |
| Stosunek ciągu do masy |
74,09 |
| Wymiary | |
| Średnica |
0,64 (jedna komora) m |
| Masa |
410 kg |
RD-0108 – radziecki silnik rakietowy. Skonstruowany przez OKB Kosberg. Silnik powstawał w latach 1959–1965. Używany do 1976.
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