The stages of a rocket going into space: The first stage of a rocket is used to acquire the acceleration of a rocket. When the fuel of the first stage is exhausted ,it detaches from the rockets and drops off. The velocity at this stage becomes the initial velocity of the second stage .Now the second stage is ignited ,the rocket gains acceleration and it's velocity foes on increasing . The removal of the surplus mass contained in the first stage helps in attaining the higher velocity .When the fuel of the second stage is exhausted ,it too detached from the rocket .Finally at the third stage , the rocket starts off with the required velocity.
Apollo 11 used a combination of liquid oxygen and hydrogen as fuel for its S-II second stage and S-IVB third stage rocket engines. The first stage of the Saturn V rocket used RP-1, a highly refined form of kerosene, along with liquid oxygen as fuel.
The bottom part of a rocket is called the "rocket stage" or "first stage." This part contains the engines and fuel necessary for liftoff and initial ascent. After its fuel is expended, it typically separates from the rest of the rocket to reduce weight for the subsequent stages.
The first stage is jettisoned, to fall back to earth, as the fuel runs out.
A rocket with 2 or more stages is called a multi-stage rocket. Each stage contains its own engines and fuel supply, and is jettisoned once its fuel is depleted to reduce the overall weight of the rocket. This allows for more efficient use of fuel and higher altitude and velocity capabilities.
That's a rocket with two stages- when the first stage (or section) runs out of fuel, it separates from the top half (second stage) and falls away, leaving that second stage to fire up, and drive the rocket higher.
That's a rocket with two stages- when the first stage (or section) runs out of fuel, it separates from the top half (second stage) and falls away, leaving that second stage to fire up, and drive the rocket higher.
If things work as planned, the first stage uses up its fuel, and falls away, while the engines of the second stage ignite and push the rocket into a higher trajectory. This point in the launch sequence is called (predictably enough!) "staging", and it is at this point that things generally go terribly wrong if they are going to. You rarely hear of a rocket in which the second stage works properly and then the THIRD stage fails. When the fuel of the second stage is exhausted, then it, too, falls away while the third stage pushes the rocket into its final orbit, or off into the solar system. This "stages falling away" part is why the USA launches its rockets from Cape Canaveral in Florida; the discarded stages fall harmlessly into the Atlantic Ocean.
If things work as planned, the first stage uses up its fuel, and falls away, while the engines of the second stage ignite and push the rocket into a higher trajectory. This point in the launch sequence is called (predictably enough!) "staging", and it is at this point that things generally go terribly wrong if they are going to. You rarely hear of a rocket in which the second stage works properly and then the THIRD stage fails. When the fuel of the second stage is exhausted, then it, too, falls away while the third stage pushes the rocket into its final orbit, or off into the solar system. This "stages falling away" part is why the USA launches its rockets from Cape Canaveral in Florida; the discarded stages fall harmlessly into the Atlantic Ocean.
The stages of a rocket going into space: The first stage of a rocket is used to acquire the acceleration of a rocket. When the fuel of the first stage is exhausted ,it detaches from the rockets and drops off. The velocity at this stage becomes the initial velocity of the second stage .Now the second stage is ignited ,the rocket gains acceleration and it's velocity foes on increasing . The removal of the surplus mass contained in the first stage helps in attaining the higher velocity .When the fuel of the second stage is exhausted ,it too detached from the rocket .Finally at the third stage , the rocket starts off with the required velocity.
If things work as planned, the first stage uses up its fuel, and falls away, while the engines of the second stage ignite and push the rocket into a higher trajectory. This point in the launch sequence is called (predictably enough!) "staging", and it is at this point that things generally go terribly wrong if they are going to. You rarely hear of a rocket in which the second stage works properly and then the THIRD stage fails. When the fuel of the second stage is exhausted, then it, too, falls away while the third stage pushes the rocket into its final orbit, or off into the solar system. This "stages falling away" part is why the USA launches its rockets from Cape Canaveral in Florida; the discarded stages fall harmlessly into the Atlantic Ocean.
Apollo 11 used a combination of liquid oxygen and hydrogen as fuel for its S-II second stage and S-IVB third stage rocket engines. The first stage of the Saturn V rocket used RP-1, a highly refined form of kerosene, along with liquid oxygen as fuel.
The first stage is jettisoned, to fall back to earth, as the fuel runs out.
If things work as planned, the first stage uses up its fuel, and falls away, while the engines of the second stage ignite and push the rocket into a higher trajectory. This point in the launch sequence is called (predictably enough!) "staging", and it is at this point that things generally go terribly wrong if they are going to. You rarely hear of a rocket in which the second stage works properly and then the THIRD stage fails. When the fuel of the second stage is exhausted, then it, too, falls away while the third stage pushes the rocket into its final orbit, or off into the solar system. This "stages falling away" part is why the USA launches its rockets from Cape Canaveral in Florida; the discarded stages fall harmlessly into the Atlantic Ocean.
The first stage is jettisoned, to fall back to earth, as the fuel runs out.
The bottom part of a rocket is called the "rocket stage" or "first stage." This part contains the engines and fuel necessary for liftoff and initial ascent. After its fuel is expended, it typically separates from the rest of the rocket to reduce weight for the subsequent stages.
A rocket with 2 or more stages is called a multi-stage rocket. Each stage contains its own engines and fuel supply, and is jettisoned once its fuel is depleted to reduce the overall weight of the rocket. This allows for more efficient use of fuel and higher altitude and velocity capabilities.