Saturn V F1 Engine Diagram

Saturn v launched apollo astronauts to the moon and the skylab space station. Five f 1 engines were clustered at the bottom of the saturn v rocket used to launch the apollo lunar missions into space. The f 1 engine was the powerplant for the first stage of the 111 meter 363 foot tall saturn v launch vehicle.

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Figure is simplified black diagram of the as 501 eds.

Saturn v f1 engine diagram. This leads to the somewhat unusual need in the case of the much larger f 1 engine for negative. The following cut away diagram of the f 1 injector shows the axially drilled holes supplying lox to the oxidizer groove rings and a fuel feed passage supplying rp 1 to the fuel ring grooves. The jupiter s s 3d engine was 100 inches tall from the exit plane to the gimbal plane and continued on up to the saturn v. Diagram of the f 1 engine.

The automafic abort initiating portion of system consists of ehe launch vehicle s rate sensing subsystem the stage. Saturn v f 1 engine diagram. 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. They were mounted to the first stage of the saturn v rocket the rocket used in the apollo missions to the moon.

Designed and manufactured by rocketdyne these engines produced over 1 5 million pounds of thrust. Saturn v s first stage had five f 1 s that created more power than 85 hoover dams. The f 1 engine the most powerful single nozzle liquid fueled rocket engine ever developed boosted the saturn v rocket off the launch pad and on to the moon during nasa s apollo program during the 1960s and 1970s. These sensors monitor the f l engine.

Saturn v rocket engines explained. It also shows the flow of fuel used to cool the circular and radial baffles. This scheme seems to have started with the jupiter missile the first abma missile with an engine with gimbal capability. A minimalist diagram of the f 1 engine the most powerful rocket engine ever made.

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 the f 1 remains the most powerful single combustion chamber liquid propellant rocket engine. Taken from saturn v quarterly report no. The purpose af the as 501 mission is to develop the saturn v launch vehicle for manned flights and to verify the adequacy of the. At an altitude of 42 miles 67 kilometers the f 1 engines shut down.

Explosive bolts fire and the severed first stage falls into the atlantic ocean.