SATURN V
Saturn V was a type of rocket developed by NASA to launch astronauts to the Moon during the Apollo missions in 1960/70.The rocket stood 363 feet tall and weighed over 6 million pounds when fully fueled.
It was made up of three stages, each with its own rocket engine and fuel supply.
It was used for a total of 13 launches, including the historic Apollo 11 mission in 1969 that landed astronauts Neil Armstrong and Buzz Aldrin on the Moon.
S-IC (BOEING)
The S-IC, or Saturn V first stage, was the largest and most powerful rocket stage ever built, designed to lift the massive Saturn V rocket off the launch pad and into orbit.
It stood 138 feet tall and was powered by five F-1 rocket engines, which generated a combined thrust of 7.5 million pounds at liftoff.
It was also responsible for providing the initial push for the rocket, burning for just over two minutes before being jettisoned and separating from the rest of the rocket.
S-II (NORTH
AMERICAN AVIATION)
The S-II was the second stage of the Saturn V rocket and was responsible for carrying the Apollo spacecraft into Earth orbit and on its trajectory to the Moon.
S-II was 81 feet long and 33 feet in diameter and was powered by five Rocketdyne J-2 engines, which burned liquid hydrogen and liquid oxygen to produce a combined thrust of over one million pounds.
The S-II was jettisoned from the Saturn V rocket once its fuel was depleted, allowing the third stage to take over and propel the spacecraft towards the Moon.
S-IVB (DOUGLAS)
The S-IVB was the third stage of the Saturn V rocket used in the Apollo missions, designed to provide the final push necessary to put the spacecraft into orbit around the Earth or on a trajectory to the Moon.
The S-IVB was powered by a single J-2 engine and could burn for up to six minutes, allowing it to accelerate the spacecraft to a speed of about 24,500 miles per hour.
On the Apollo 8 mission, the S-IVB intentionally crashed into the Moon to generate seismic data for scientific study.
INSTRUMENT UNIT
(IBM)
The Instrument Unit (IU) was a critical component of the Saturn V rocket, located at the top of the third stage.
It included gyroscopes and accelerometers, which provided information on the rocket's position, velocity, and attitude, and allowed the guidance system to make necessary adjustments.
The IU was also responsible for initiating stage separation and other critical events during the launch sequence, but not only that, but it also played a crucial role in the success of the Apollo missions, providing the precise guidance and control necessary to achieve lunar orbit and successfully return to Earth.
LUNAR MODULE (GRUMMAN)
The Lunar Module was a spacecraft designed to land on the Moon and provide a base for the astronauts during their time on the lunar surface.
It consisted of two parts, the descent stage and the ascent stage:The descent stage contained the engine and fuel necessary to land on the Moon, as well as living quarters and equipment for the astronauts.
The ascent stage was designed to take the astronauts back into lunar orbit and included the engine and fuel necessary for the return journey to the Command Module.
SERVICE MODULE
(NORTH AMERICAN)
The Service Module (SM) was a critical component of the Apollo spacecraft, attached to the Command Module and responsible for providing propulsion, power, and life support systems during the mission.
It included the main engine, which provided the necessary thrust to enter and exit lunar orbit, as well as a number of smaller engines used for attitude control and maneuvering.
The SM also housed the fuel and oxygen supplies necessary for the mission and provided electrical power and environmental control systems for the crew.
COMMAND MODULE
The Command Module (CM) was the crew compartment of the Apollo spacecraft, located at the top of the Saturn V rocket and responsible for carrying the three astronauts into space and back safely to Earth.
The CM contained living quarters for the crew, including sleeping bunks, a galley, and waste management systems.
It was also equipped with communication and navigation systems, allowing the crew to communicate with mission control and track their position during the mission.
LAUNCH ESCAPE
SYSTEM
The Saturn V rocket was equipped with a launch escape system designed to protect the crew in the event of a catastrophic failure during the launch.
The system consisted of a tower mounted atop the crew module that contained three solid-fueled rockets capable of propelling the module away from the rocket and towards safety.
If a problem was detected during launch, the system would be triggered, and the rockets would ignite, carrying the crew module away from the rocket and into the air where the parachutes would deploy to bring the module back to Earth safely.