cross section of a space launcher (Saturn V) [2]
				   		Saturn V served as the launcher for the U.S. Apollo lunar exploration program.
				
 
					
					
					
						payload 
						Includes the Apollo craft, the lunar module and the third stage; the latter, after being placed in Earth’s orbit, soars toward the Moon.
				  	
 
					
						third stage 
						At an altitude of 92 mi, the third-stage engine begins to run, allowing the launcher to place itself in orbit before making its way toward the Moon.
				  	
 
					
						second stage 
						At an altitude of 38.8 mi, the five second-stage engines ignite, burning for 6 min. 30 sec. before they are jettisoned.
				  	
 
					
						first stage 
						Equipped with five F-1 engines that give the launcher the thrust it needs to leave the launchpad; jettisoned after 2 min. 30 sec. of flight.
				  	
 
					
						F-1 engine 
						The first stage is equipped with five; it provides thrust using kerosene-liquid oxygen combustion.
				  	
 
					
						nozzle 
						The end portion of a rocket from which combustion gases escape, thereby creating the thrust needed to propel the craft.
				  	
 
					
						stabilizing fin 
						Fins located on either side of the launcher, serving to stabilize it.
				  	
 
					
						service module 
						Houses the main propulsion system and supplies energy, electricity, water and other provisions.
						
				  	 
					
						command module 
						Capsule inhabited by the crew during most of an Apollo mission; the only part of the vehicle to return to Earth.
						
				  	 
					
						launch escape system 
						Makes it possible, in the event of damage, to separate the command module from the rest of the launcher and to pull it.
				  	
 
					
						fuel transfer pipe 
						Pipe through which liquid oxygen is sent to the rocket engines.
				  	
 
					
						kerosene tank 
						Kerosene, burned on contact with liquid oxygen, serves as fuel for F-1 engines.
				  	
 
					
						liquid oxygen tank baffle 
						Serves to limit the movement of liquid oxygen inside the tank.
				  	
 
					
						liquid oxygen tank 
						Contains liquid oxygen used to burn kerosene.
				  	
 
					
						liquid hydrogen tank 
						Hydrogen, burned on contact with liquid oxygen, serves as engine fuel.
				  	
 
					
						J-2 engine 
						The second and third stages are equipped with J-2 engines; these provide thrust using liquid oxygen-hydrogen combustion.
				  	
 
					
						helium sphere 
						Helium is used to pressurize the oxygen tank.
				  	
 
					
						instrument unit 
						The brain of the rocket; includes the computers and all of the electronic equipment that controls the rocket during its launch.
				  	
 
					
						lunar module 
						Inhabited section of the craft; enabled two men to walk on the Moon and spend a few days there before returning to dock with the Apollo capsule.