Rocketdyne F-1
| Use attributes for filter ! | |
| Manufacturers | Rocketdyne |
|---|---|
| Thrust-to-weight ratio | 94. 1 |
| Thrust (vac.) | 1,746,000 lbf (7,770 kN) |
| Thrust (SL) | 1,522,000 lbf (6,770 kN) |
| Chamber pressure | 70 bars (1,015 psi; 7 MPa) |
| Diameter | 12. 2 feet (3. 7 m) |
| Date of Reg. | |
| Date of Upd. | |
| ID | 2351580 |
About Rocketdyne F-1
The F-1 is a gas generator-cycle rocket engine developed in the United States by Rocketdyne in the late 1950s and used in the Saturn V rocket in the 1960s and early 1970s. Five F-1 engines were used in the S-IC first stage of each Saturn V, which served as the main launch vehicle of the Apollo program.
Rocketdyne F-1 Photos
