XLR81-BA-7
| Kraj pochodzenia |  Stany Zjednoczone |
|---|---|
| Projektant | Bell Aircraft Corporation |
| Wykorzystanie | Agena B |
| Materiały napędowe | kwas azotowy i UDMH |
| Pierwszy lot | 1960 |
| Ostatni lot | 1967 |
| Osiągi | |
| Siła ciągu w próżni | 71,2 kN |
| Impuls właściwy w próżni | 285 s |
| Maks. czas działania | 240 s |
| Parametry | |
| Komory spalania | 1 |
| Ciśnienie w komorze | 10 bar |
| Stosunek ciągu do masy | 55,82 |
| Wymiary | |
| Średnica | 1,52 m |
| Masa | 130 kg |
XLR81-BA-7 – Bell 8081 – amerykański silnik rakietowy. Był używany w członie rakietowym Agena B. Odnotowano 102 użycia tego silnika.
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