XLR81-BA-5
| Kraj pochodzenia |  Stany Zjednoczone |
|---|---|
| Projektant | Bell Aircraft Corporation |
| Wykorzystanie | Agena A |
| Materiały napędowe | kwas azotowy i UDMH |
| Pierwszy lot | 1959 |
| Ostatni lot | 1961 |
| Osiągi | |
| Siła ciągu w próżni | 68,9 kN |
| Impuls właściwy w próżni | 276 s |
| Maks. czas działania | 120 s |
| Parametry | |
| Komory spalania | 1 |
| Ciśnienie w komorze | 10 bar |
| Stosunek ciągu do masy | 55,36 |
| Wymiary | |
| Długość | 2,16 m |
| Średnica | 1,52 m |
| Masa | 127 kg |
XLR81-BA-5 (także: Bell 8048) – amerykański silnik rakietowy. Był używany w członie Agena A rakiet Thor Agena A i Atlas Agena A.
Używano również wariantu silnika oznaczonego XLR81-BA-3.
Bibliografia
- Encyclopedia Astronautica. [dostęp 2010-11-28].
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