Also known as Rocketdyne F-1, Rocketdyne F1
US-amerikanisches Raketentriebwerk
Key facts
- Country of origin
- United States
- First flight
- November 9, 1967 ( 1967-11-09 ) ( Apollo 4 )
- Last flight
- May 14, 1973 ( 1973-05-14 ) ( Skylab 1 )
- Designer
- Rocketdyne
- Manufacturer
- Rocketdyne
- Associated launch vehicle span lv
- Saturn V , Saturn C-3 , Saturn C-4 , Saturn C-8
- Propellant
- LOX / RP-1
- Mixture ratio
- 2.27:1, (69% LOX, 31% RP-1)
- Cycle
- Gas-generator
- Thrust vacuum
- 7,770 kN (1,746,000 lbf)
- Thrust sea level
- 6,770 kN (1,522,000 lbf)
- Thrust to weight ratio
- 94.1:1
- Chamber pressure
- 70 bar (1,015 psi; 7 MPa)
- Specific impulse vacuum
- 304 s (2.98 km/s)
- Specific impulse sea level
- 263 s (2.58 km/s)
- Mass flow
- LOX : 1,789 kg/s (3,945 lb/s) RP-1 : 788 kg/s (1,738 lb/s)
- Burn time
- 150 to 163 seconds
- Length
- 5.6 m (18.5 ft)
via Wikipedia infobox
Wikidata facts
- Subclass of
- rocket engine
- Country of origin
- United States
- Diameter
- 3.76
- Mass
- 8391
- Manufacturer
- Rocketdyne
- Image
- F-1 rocket engine at KSC.jpg
- Height
- 5.79
Show 4 more facts
- source of energy
- RP-1
- Commons category
- F-1 (rocket engine)
- specific impulse by weight
- 263
- maximum thrust
- 1522000
Sources (3)
via Wikidata · CC0