| Beal Aerospace | BA-2 | |||
|
Overall Vehicle |
Operational | from | ||
| to | ||||
| Orbital flights | 0 | |||
| Payload weight | t | LEO | 16.96 | |
| Gross liftoff weight | t | 1,058.6 | ||
| Gross propellant weight | t | 976.4 | ||
| Total length | m | 64.62 | ||
| Max. diameter (span) | m | |||
| Total liftoff thrust (s.l.) | kN | 11,980 | ||
| Total impulse (vac) | MN*s | 2,544.5 | ||
|
Fairing |
Total length | m | 12.50 | |
| Diameter | m | 6.22 | ||
| Total weight | t | 2.400 | ||
| Stage 3 |
Name |
|||
| Length | m | (8.20) | ||
| Diameter | m | 6.22 | ||
| Liftoff weight | t | 42.85 | ||
| Propellant weight | t | 40.00 | ||
| Engines |
BA-44 |
|||
| Propellant |
Kerosene/H2O2 |
|||
| Total thrust (vac) | kN | 196.2 | ||
| Specific impulse (vac) | N*s/kg | 2942 | ||
| Burn time | s | 600 | ||
| Total impulse (vac) | MN*s | 117.7 | ||
|
Stage 2 |
Name | |||
| Length | m | (18.78) | ||
| Diameter | m | 6.22 | ||
| Liftoff weight | t | 229.4 | ||
| Propellant weight | t | 214.7 | ||
| Engines | BA-810 | |||
| Propellant |
Kerosene/H2O2 |
|||
| Total thrust (vac) | kN |
3,599 |
||
| Specific impulse (vac) | N*s/kg |
2765 |
||
| Burn time | s |
165 |
||
| Total impulse (vac) | MN*s |
593.7 |
||
|
Stage 1 |
Name | |||
| Length | m | 38.76 (31.58) | ||
| Diameter | m | 6.22 | ||
| Liftoff weight | t | 767.0 | ||
| Propellant weight | t | 721.7 | ||
| Engines | BA-3200 | |||
| Propellant | Kerosene/H2O2 | |||
| Total thrust (s.l.) | kN | 11,980 | ||
| Specific impulse (s.l.) | N*s/kg | 2158 | ||
| Burn time | s | 130 | ||
| Total impulse (vac) | MN*s | 1,833.1 | ||