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 |