Propulsion "New Shepard"
Version |
Propellant |
Engine |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp (vac) |
kN | N*s/kg | kN | N*s/kg | t | sec | t/s | MN*sec | |||
"Goddard" PM-1 | HP |
BE-1 (9) |
88.1 | |||||||
"New Shepard" PM-2 | Kerosene/HP |
BE-2 (3) |
413.8 | 2297 | 471.6 | 2618 | ? | 0.1801 | ? | |
"New Shepard" PM-3 | LH2/LOX |
BE-3 (1) |
489.3 | 3530 | 550.5 | 3972 | 18.57* | 134* | 0.1386 | 84.8 |
2.77** | 20** |
*
Ascent phase
** Descent phase
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