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(Redirected from Multi-stage rocket)
A 'multistage' (or 'multi-stage') 'rocket' is a rocket that uses
two or more ''stages'', each of which contains its own engines and propellant. A ''stacked'' stage is mounted on top of another stage; a ''parallel'' stage is attached next to another stage. The result is effectively two or more rockets stacked on top of or attached next to each other. Taken together these are sometimes called a launch vehicle. Two stage rockets are quite common, but rockets with as many as five separate stages have been successfully launched.
By jettisoning stages when they run out of propellant, the mass of the remaining rocket is decreased. This ''staging'' allows the thrust of the remaining stages to more easily accelerate the rocket to its final speed and height.
In stacked staging schemes, the 'first stage' is at the bottom and is usually the largest, the 'second stage' is above it and is usually the next largest. Subsequent 'upper stages' are above those. In parallel staging schemes solid or liquid rocket boosters are used to assist with lift-off. These are sometimes referred to as 'stage 0'. In the typical case, the first stage and booster engines fire to propel the entire rocket upwards. When the boosters run out of fuel, they detached from the rest of the rocket (usually with some kind of small explosive charge) and fall away. The first stage then burns to completion and falls off. This leaves a smaller rocket, with the second stage on the bottom, which then fires. This process is repeated until the final stage's motor burns to completion.
The Space shuttle has two large boosters and is not Single-stage-to-orbit (SSTO).
The main reason for multi-stage rockets and boosters is that once the fuel is burnt, the space and structure which contained it and the motors themselves are useless and only add weight to the vehicle which slows down its future acceleration. By dropping the stages which are no longer useful, the rocket lightens itself. The thrust of the future stages is able to provide more acceleration than if the earlier stages were still attached, or than a single, large rocket would be capable of. When a stage drops off, the rest of the rocket is still travelling near to the speed that the whole assembly reached at burn-out time. This means that it needs less total fuel to reach a given velocity and/or altitude.
A further advantage is that each stage can use a different type of rocket motor, with each stage/motor tuned for the conditions in which it will operate. Thus the lower stage motors are designed for use at atmospheric pressure, while the upper stages can use motors suited to near vacuum conditions. Lower stages tend to require more structure than upper as they need to bear their own weight plus that of the stages above them, optimizing the structure of each stage decreases the weight of the total vehicle and provides further advantage.
On the downside, staging requires the vehicle to lift motors which are not being used until later, as well as making the entire rocket more complex and harder to build. Nevertheless the savings are so great that every rocket currently used to deliver a payload into orbit uses staging.
In more recent times the usefulness of the technique has come into question due to developments in technology. In the case of the Space Shuttle the costs of space launches appear to mostly composed of the operational costs of the people involved (as opposed to fuel or equipment), reducing these costs appears to be the best way to lower the overall launch costs. New technology that is mainly in the theoretical and developmental stages is being looked at to lower the costs of launch vehicles. More information can be found on single stage to orbit designs that do not have separate stages.
From an illustration and description in the 14th century Chinese ''Huolongjing'' of Jiao Yu is the oldest known multistage rocket; this was the 'fire-dragon issuing from the water' (huo long chu shui), used mostly by the Chinese navy.[1] It was a two-stage rocket that had carrier or booster rockets that would eventually burn out, yet before they did they automatically ignited a number of smaller rocket arrows that were shot out of the front end of the missile, which was shaped like a dragon's head with an open mouth. This multi-stage rocket may be considered the ancestor to the modern exocet. The historian Joseph Needham points out that the written material and depicted illustration of this rocket come from the oldest stratum of the ''Huolongjing'', which can be dated roughly 1300-1350 AD (from the book's part 1, chapter 3, page 23).
The earliest experiments with multistage rockets in Europe were made by Austrian Conrad Haas, the arsenal master of the town of Sibiu, Transylvania (now in Romania) in 1551.
This concept was developed independently by at least four individuals:
★ the Polish Kazimierz Siemienowicz
★ the Russian Konstantin Tsiolkovsky
★ the American Robert Goddard
★ the ethnically German, Transylvanian-born Hermann Oberth.
★ Bumper Project
★ Conrad Haas
★ Reusable launch system
★ Single-stage to orbit
The second stage of a Minuteman III rocket
A 'multistage' (or 'multi-stage') 'rocket' is a rocket that uses
two or more ''stages'', each of which contains its own engines and propellant. A ''stacked'' stage is mounted on top of another stage; a ''parallel'' stage is attached next to another stage. The result is effectively two or more rockets stacked on top of or attached next to each other. Taken together these are sometimes called a launch vehicle. Two stage rockets are quite common, but rockets with as many as five separate stages have been successfully launched.
By jettisoning stages when they run out of propellant, the mass of the remaining rocket is decreased. This ''staging'' allows the thrust of the remaining stages to more easily accelerate the rocket to its final speed and height.
In stacked staging schemes, the 'first stage' is at the bottom and is usually the largest, the 'second stage' is above it and is usually the next largest. Subsequent 'upper stages' are above those. In parallel staging schemes solid or liquid rocket boosters are used to assist with lift-off. These are sometimes referred to as 'stage 0'. In the typical case, the first stage and booster engines fire to propel the entire rocket upwards. When the boosters run out of fuel, they detached from the rest of the rocket (usually with some kind of small explosive charge) and fall away. The first stage then burns to completion and falls off. This leaves a smaller rocket, with the second stage on the bottom, which then fires. This process is repeated until the final stage's motor burns to completion.
The Space shuttle has two large boosters and is not Single-stage-to-orbit (SSTO).
A two-stage Delta III with nine solid rocket booster attached. (Photo courtesy Boeing)
| Contents |
| Advantages |
| Disadvantages |
| Development |
| Alternatives to rockets |
| See also |
Advantages
The main reason for multi-stage rockets and boosters is that once the fuel is burnt, the space and structure which contained it and the motors themselves are useless and only add weight to the vehicle which slows down its future acceleration. By dropping the stages which are no longer useful, the rocket lightens itself. The thrust of the future stages is able to provide more acceleration than if the earlier stages were still attached, or than a single, large rocket would be capable of. When a stage drops off, the rest of the rocket is still travelling near to the speed that the whole assembly reached at burn-out time. This means that it needs less total fuel to reach a given velocity and/or altitude.
A further advantage is that each stage can use a different type of rocket motor, with each stage/motor tuned for the conditions in which it will operate. Thus the lower stage motors are designed for use at atmospheric pressure, while the upper stages can use motors suited to near vacuum conditions. Lower stages tend to require more structure than upper as they need to bear their own weight plus that of the stages above them, optimizing the structure of each stage decreases the weight of the total vehicle and provides further advantage.
Disadvantages
Cutaway drawings showing three multi-stage rockets (Image courtesy NASA)
An artist's conception of the separation of the S1-B stage of a Saturn IB rocket (Image courtesy NASA)
The second stage being lowered into the first stage of a Saturn V rocket (Photo courtesy NASA)
A diagram of the second stage and how it fits into the complete rocket (Image courtesy NASA)
On the downside, staging requires the vehicle to lift motors which are not being used until later, as well as making the entire rocket more complex and harder to build. Nevertheless the savings are so great that every rocket currently used to deliver a payload into orbit uses staging.
In more recent times the usefulness of the technique has come into question due to developments in technology. In the case of the Space Shuttle the costs of space launches appear to mostly composed of the operational costs of the people involved (as opposed to fuel or equipment), reducing these costs appears to be the best way to lower the overall launch costs. New technology that is mainly in the theoretical and developmental stages is being looked at to lower the costs of launch vehicles. More information can be found on single stage to orbit designs that do not have separate stages.
Development
From an illustration and description in the 14th century Chinese ''Huolongjing'' of Jiao Yu is the oldest known multistage rocket; this was the 'fire-dragon issuing from the water' (huo long chu shui), used mostly by the Chinese navy.[1] It was a two-stage rocket that had carrier or booster rockets that would eventually burn out, yet before they did they automatically ignited a number of smaller rocket arrows that were shot out of the front end of the missile, which was shaped like a dragon's head with an open mouth. This multi-stage rocket may be considered the ancestor to the modern exocet. The historian Joseph Needham points out that the written material and depicted illustration of this rocket come from the oldest stratum of the ''Huolongjing'', which can be dated roughly 1300-1350 AD (from the book's part 1, chapter 3, page 23).
The earliest experiments with multistage rockets in Europe were made by Austrian Conrad Haas, the arsenal master of the town of Sibiu, Transylvania (now in Romania) in 1551.
This concept was developed independently by at least four individuals:
★ the Polish Kazimierz Siemienowicz
★ the Russian Konstantin Tsiolkovsky
★ the American Robert Goddard
★ the ethnically German, Transylvanian-born Hermann Oberth.
Alternatives to rockets
See also
★ Bumper Project
★ Conrad Haas
★ Reusable launch system
★ Single-stage to orbit
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