S-IC

first stage of the Saturn V rocket.
Saturn S-IC

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Wikimedia, Wikidata
liquid-propellant rocket, United States of America,

Freebase entry^@

At the Marshall Space Flight Center (MSFC), the fuel tank assembly for the Saturn V S-IC-T (static test stage) fuel tank assembly is mated to the liquid oxygen (LOX) tank in building 4705.

Engineers and technicians at the Marshall Space Flight Center were installing an F-I engine on the Saturn V S-IC (first) stage thrust structure in building 4705.

Marshall Space Flight Center successfully conducted hydrostatic testing on the Saturn V S-IC (first) stage fuel tank. The first stage was powered by five F-1 engines, that used liquid oxygen and kerosene as its propellant.

Pearl River barge transporting Saturn V S-IC from MTO

Pearl River barge transporting Saturn V S-I on East Pearl River

SaturnVThrust2

SaturnV S-IC

SaturnV S-IC (cropped)

Saturn V S-IC cutaway

The components of the Saturn V booster (S-IC stage) fuel tank are shown in this photograph.

The fuel tank assembly for the Saturn V S-IC (first) stage arrived at the Marshall Space Flight Center, building 4707, for mating to the liquid oxygen tank. The fuel tank carried kerosene as its fuel.

The fuel tank assembly of the Saturn V S-IC (first) stage is readied to be mated to the liquid oxygen tank at the Marshall Space Flight Center. The fuel tank carried kerosene as its fuel.

The fuel tank assembly of the Saturn V S-IC (first) stage supported with the aid of a C frame on the transporter was readied to be transported to the Marshall Space Flight Center, building 4705. The fuel tank carried kerosene (RP-1) as its fuel.

This image illustrates technicians working on a full scale engineering mock-up of a Saturn V S-IC stage thrust structure nearing completion at the Manufacturing Engineering Laboratory at Marshall Space Flight Center.

This image shows the Saturn V S-IC-T stage (S-IC static test article) fuel tank being attached to the thrust structure in the vehicle assembly building at the Marshall Space Flight Center (MSFC).

This is a picture of the assembled liquid oxygen (LOX) tank for the Saturn V S-IC (first) stage, with A-frame, that arrived to be mated to the fuel tank at a later date at the Marshall Space Flight Center, building 4705.

This photograph depicts Marshall Space Flight Center employees, James Reagin, machinist (top); Floyd McGinnis, machinist; and Ernest Davis, experimental test mechanic (foreground), working on a mock up of the S-IC thrust structure.

This photograph depicts a forward skirt being placed on the liquid oxygen tank for Saturn V S-IC (first) stage in the Manufacturing Engineering Laboratory at the Marshall Space Flight Center.

This photograph shows a Saturn V first stage (S-1C). This stage was assembled at the Manufacturing Engineering Laboratory at NASA's Marshall Space Flight Center.

This photograph shows how the fuel tank assembly and the liquid oxygen tank for the Saturn V S-IC (first) stage are placed side by side prior to commencement of the mating of the two stages in the Marshall Space Flight Center, building 4705.

This photograph shows the components for the Saturn V S-IC stage fuel tank assembly in the Manufacturing Engineering Laboratory, building 4707, at the Marshall Space Flight Center (MSFC).

This photograph shows the fuel tank assembly for the Saturn V S-IC (first) stage being transported to the Marshall Space Flight Center, building 4705 for mating to the liquid oxygen (LOX) tank. The fuel tank carried kerosene (RP-1) as its fuel.

This small group of unidentified officials is dwarfed by the gigantic size of the Saturn V first stage (S-1C) at the shipping area of the Manufacturing Engineering Laboratory at Marshall Space Flight Center in Huntsville, Alabama.

Type	Date	Description	Source

link		Freebase entry^@	Wikidata
image	1964	At the Marshall Space Flight Center (MSFC), the fuel tank assembly for the Saturn V S-IC-T (static test stage) fuel tank assembly is mated to the liquid oxygen (LOX) tank in building 4705.	Wikimedia
image	1965	Engineers and technicians at the Marshall Space Flight Center were installing an F-I engine on the Saturn V S-IC (first) stage thrust structure in building 4705.	Wikimedia
image	1963	Marshall Space Flight Center successfully conducted hydrostatic testing on the Saturn V S-IC (first) stage fuel tank. The first stage was powered by five F-1 engines, that used liquid oxygen and kerosene as its propellant.	Wikimedia
image		Pearl River barge transporting Saturn V S-IC from MTO	Wikimedia
image		Pearl River barge transporting Saturn V S-I on East Pearl River	Wikimedia
image		SaturnVThrust2	Wikimedia
image		SaturnV S-IC	Wikimedia
image		SaturnV S-IC (cropped)	Wikimedia
image		Saturn V S-IC cutaway	Wikimedia
image	1964	The components of the Saturn V booster (S-IC stage) fuel tank are shown in this photograph.	Wikimedia
image	1964	The fuel tank assembly for the Saturn V S-IC (first) stage arrived at the Marshall Space Flight Center, building 4707, for mating to the liquid oxygen tank. The fuel tank carried kerosene as its fuel.	Wikimedia
image	1964	The fuel tank assembly of the Saturn V S-IC (first) stage is readied to be mated to the liquid oxygen tank at the Marshall Space Flight Center. The fuel tank carried kerosene as its fuel.	Wikimedia
image	1964	The fuel tank assembly of the Saturn V S-IC (first) stage supported with the aid of a C frame on the transporter was readied to be transported to the Marshall Space Flight Center, building 4705. The fuel tank carried kerosene (RP-1) as its fuel.	Wikimedia
image	1963	This image illustrates technicians working on a full scale engineering mock-up of a Saturn V S-IC stage thrust structure nearing completion at the Manufacturing Engineering Laboratory at Marshall Space Flight Center.	Wikimedia
image	1964	This image shows the Saturn V S-IC-T stage (S-IC static test article) fuel tank being attached to the thrust structure in the vehicle assembly building at the Marshall Space Flight Center (MSFC).	Wikimedia
image	1964	This is a picture of the assembled liquid oxygen (LOX) tank for the Saturn V S-IC (first) stage, with A-frame, that arrived to be mated to the fuel tank at a later date at the Marshall Space Flight Center, building 4705.	Wikimedia
image	1963	This photograph depicts Marshall Space Flight Center employees, James Reagin, machinist (top); Floyd McGinnis, machinist; and Ernest Davis, experimental test mechanic (foreground), working on a mock up of the S-IC thrust structure.	Wikimedia
image	1964	This photograph depicts a forward skirt being placed on the liquid oxygen tank for Saturn V S-IC (first) stage in the Manufacturing Engineering Laboratory at the Marshall Space Flight Center.	Wikimedia
image	1960	This photograph shows a Saturn V first stage (S-1C). This stage was assembled at the Manufacturing Engineering Laboratory at NASA's Marshall Space Flight Center.	Wikimedia
image	1964	This photograph shows how the fuel tank assembly and the liquid oxygen tank for the Saturn V S-IC (first) stage are placed side by side prior to commencement of the mating of the two stages in the Marshall Space Flight Center, building 4705.	Wikimedia
image	1964	This photograph shows the components for the Saturn V S-IC stage fuel tank assembly in the Manufacturing Engineering Laboratory, building 4707, at the Marshall Space Flight Center (MSFC).	Wikimedia
image	1964	This photograph shows the fuel tank assembly for the Saturn V S-IC (first) stage being transported to the Marshall Space Flight Center, building 4705 for mating to the liquid oxygen (LOX) tank. The fuel tank carried kerosene (RP-1) as its fuel.	Wikimedia
image	1960	This small group of unidentified officials is dwarfed by the gigantic size of the Saturn V first stage (S-1C) at the shipping area of the Manufacturing Engineering Laboratory at Marshall Space Flight Center in Huntsville, Alabama.	Wikimedia

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