Rocketdyne F-1

The F-1 is a rocket engine developed by Rocketdyne and used in the Saturn V. Five F-1 engines were used in the S-IC first stage of each Saturn V, which served as the main launch vehicle in the Apollo program. The F-1 is still the most powerful single-chamber liquid-fueled rocket engine developed (the RD-170 is more powerful but it has 4 chambers). The F-1 was originally developed by Rocketdyne to meet a 1955 US Air Force requirement for a very la... more

Spaceflight

Status:

Used in rocket stages:

Rocket Stage Number Thrust (newtons) Burn Time (seconds) Fuels
  • 1
  • 34,020,000 N (246067130 pdl )
  • 2 min 30 s
  • 1
  • 34,020,000 N (246067130 pdl )
  • 2 min 30 s
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Manufactured by:

Designed by:

Design period:

Start End
  • 1957
  • 1967

Use period:

Start End
  • 1967
  • 1973

Diameter:

  • 3.7 m (12 ft )

Height:

  • 5.6 m (18 ft )

Thrust (vacuum):

  • 7,740,000 N (55983530 pdl )

Thrust (sea level):

  • 6,700,000 N (48461190 pdl )

Isp (vacuum):

  • 5 min 4 s

Isp (sea level):

  • 4 min 20 s

Dry mass:

  • 8,353 kg (18420 lb )

Wet mass:

  • 9,115 kg (20100 lb )

Engine cycle:

Fuel:

Oxidizer:

Oxidizer/fuel ratio:

  • 2.27

Expansion ratio:

  • 16

Chamber pressure:

  • 70 bar (1000 psi )

Number of chambers:

  • 1
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