Mission Profile: Apollo 11 // Launch Complex 39A

SATURN V

"We choose to go to the moon."

— J.F. Kennedy // Rice University, 1962

Height
363 FT
Thrust
7.6M LBS
Mass
6.5M LBS
Payload (TLI)
107,000 LBS
REF: DR. VON BRAUN
Propulsion System

The F-1 Engines

Five engines. 7.5 million pounds of thrust.

The F-1 remains the most powerful single-chamber liquid-fueled rocket engine ever developed. At liftoff, the Saturn V generated more power than 85 Hoover Dams.

> FUEL CONSUMPTION: 15 TONS / SEC
> BURN TIME: 165 SECONDS

Staging Profile

CONFIG: APOLLO 11 // LAUNCH MASS: 6.5M LBS

Saturn V Schematic

Stage III: S-IVB

TLI BURN

The final push. A single J-2 engine reignited in orbit to send the crew out of Earth's gravity and towards the Moon (Trans-Lunar Injection).

THRUST 225,000 LBF
FUEL LH2 / LOX
BURN TIME 475 SEC

Stage II: S-II

ATMOSPHERIC EXIT

The workhorse of the ascent. Five J-2 engines burning liquid hydrogen powered the stack through the upper atmosphere to reach orbital velocity.

THRUST 1,000,000 LBF
FUEL LH2 / LOX
BURN TIME 360 SEC

Stage I: S-IC

THE BOOSTER

The brute force. Five massive F-1 engines consuming 15 tons of fuel per second to lift the 6.5 million pound vehicle off the ground.

THRUST 7,600,000 LBF
FUEL RP-1 / LOX
BURN TIME 168 SEC