User:Audin
From Wikipedia, the free encyclopedia
Evolving standard launch vehicle stat table.
| Saturn V | ||
|---|---|---|
![]() Saturn V launching Apollo 15. |
||
| Stages | ||
| 1 | Engines | |
| Thrust | lbs | |
| ISP | sec | |
| Burn time | ~ sec | |
| Fuels | RP-1/LOX | |
| 2 | Engines | |
| Thrust | lbs | |
| Burn time | ~ sec | |
| Fuels | LH2/LOX | |
| 3 | Engines | |
| Thrust | lbs | |
| Burn time | ~ sec | |
| Fuels | LH2/LOX | |
| Three stage version | ||
| Payload to LEO | 118,000 kg | |
| Payload to TLI | 47,000 kg | |
| Saturn V | ||
|---|---|---|
![]() Saturn V launching Apollo 15. |
||
| Stages | 3 | |
| 1 | Engines | |
| Thrust | lbs | |
| ISP | sec | |
| Burn time | ~ sec | |
| Fuels | RP-1/LOX | |
| 2 | Engines | |
| Thrust | lbs | |
| ISP | sec | |
| Burn time | ~ sec | |
| Fuels | RP-1/LOX | |
| 3 | Engines | |
| Thrust | lbs | |
| ISP | sec | |
| Burn time | ~ sec | |
| Fuels | RP-1/LOX | |
| Three stage version | ||
| Payload to LEO | 118,000 kg | |
| Payload to TLI | 47,000 kg | |
| Saturn V | ||
|---|---|---|
![]() Saturn V launching Apollo 15. |
||
| Stages | ||
| 1 | Engines | |
| Thrust | lbs | |
| ISP | sec | |
| Burn time | ~ sec | |
| Fuels | RP-1/LOX | |
| 2 | Engines | |
| Thrust | lbs | |
| Burn time | ~ sec | |
| Fuels | LH2/LOX | |
| 3 | Engines | |
| Thrust | lbs | |
| Burn time | ~ sec | |
| Fuels | LH2/LOX | |
| Three stage version | ||
| Payload to LEO | 118,000 kg | |
| Payload to TLI | 47,000 kg | |


