Water rocket

Not to be confused with bottle rockets powered by black powder.
Water rocket launch

A water rocket is a type of model rocket using water as its reaction mass. Such a rocket is typically made from a used plastic soft drink bottle. The water is forced out by a pressurized gas, typically compressed air. Like all rocket engines, it operates on the principle of Newton's third law of motion.

Operation

Simplified animation of how a water rocket works. 1) A bubble of compressed air is added and pressurizes the contents of the bottle. 2) The bottle is released from the pump. 3) The water is pushed out through the nozzle by the compressed air. 4) The bottle moves away from the water because it follows Newton's Third Law.

The bottle is partly filled with water and sealed. The bottle is then pressurized with a gas, usually air compressed from a bicycle pump, air compressor, or cylinder up to 125 psi, but sometimes CO2 or nitrogen from a cylinder.

Water and gas are used in combination, with the gas providing a means to store potential energy, as it is compressible, and the water increasing the propellant mass fraction and providing greater force when ejected from the rocket's nozzle. Sometimes additives are combined with the water to enhance performance in different ways. For example: salt can be added to increase the density of the reaction mass resulting in a higher specific impulse. Soap is also sometimes used to create a dense foam in the rocket which lowers the density of the expelled reaction mass but increases the duration of thrust. It is speculated that foam acts as a compressible fluid and enhances the thrust when used with De Laval nozzles.

Launching a water rocket. The rocket is in its peak with no water inside it.

The seal on the nozzle of the rocket is then released and rapid expulsion of water occurs at high speeds until the propellant has been used up and the air pressure inside the rocket drops to atmospheric pressure. There is a net force created on the rocket in accordance with Newton's third law. The expulsion of the water thus can cause the rocket to leap a considerable distance into the air.

In addition to aerodynamic considerations, altitude and flight duration are dependent upon the volume of water, the initial pressure, the rocket nozzle's size, and the unloaded weight of the rocket. The relationship between these factors is complex and several simulators have been written to explore these and other factors.[1][2][3]

Often the pressure vessel is built from one or more used plastic soft drink bottles, but polycarbonate fluorescent tube covers, plastic pipes, and other light-weight pressure-resistant cylindrical vessels have also been used.

Elements

Bottle

Two multi-bottle rockets with a cat for scale.
A larger multi bottle rocket with cylindrical fins.

The standard bottle used is a single polyethylene terephthalate two-liter bottle as used for carbonated soft drinks.

Multi-bottle rockets are created by joining two or more bottles in any of several different ways; bottles can be connected via their nozzles, by cutting them apart and sliding the sections over each other, or by connecting them opening to bottom, making a chain to increase volume. This adds complexity and the increased volume leads to increased weight - but this should be offset by an increase in the duration of the thrust of the rocket.

Multi-stage rockets are much more complicated. They involve two or more rockets stacked on top of each other, designed to launch while in the air, much like the multi-stage rockets that are used to send payloads into space. Techniques to time the launches in correct order and at the right time vary, but include the "crushing-sleeve" method.[4]

Gas

Several methods for pressurizing a water rocket are used including:

Nozzles

Water rocket nozzles differ from conventional combustion rocket nozzles in that they do not have a divergent section such as in a De Laval nozzle. Because water is essentially incompressible the divergent section does not contribute to efficiency and actually can make performance worse.

There are two main classes of water rocket nozzles:

The size of the nozzle affects the thrust produced by the rocket. Larger diameter nozzles provide faster acceleration with a shorter thrust phase, while smaller nozzles provide lower acceleration with a longer thrust phase.

It can be shown that the equation for the instantaneous thrust of a nozzle is simply:[6]

where is the thrust, is the pressure and is area of the nozzle.

Fins

As the propellant level in the rocket goes down, the centre of mass initially moves downwards before finally moving upwards again as the propellant is depleted. This initial movement reduces stability and can cause water rockets to start tumbling end over end, greatly decreasing the maximum speed and thus the length of glide (time that the rocket is flying under its own momentum).

To lower the centre of pressure and add stability, fins or other stabilizers can be added which bring the centre of drag further back, well behind the centre of mass at all times. Stabilizers of any sort are normally placed near the back of the bottle where the center of mass is found. The increase in stability which well-designed fins give is worth the extra drag, and helps to maximize the height to which the rocket will fly.[7]

Landing systems

Stabilizing fins cause the rocket to fly nose-first which will give significantly higher speed, but they will also cause it to fall with a significantly higher velocity than it would if it tumbled to the ground, and this may damage the rocket or whomever or whatever it strikes upon landing.

Some water rockets have parachute or other recovery system to help prevent problems. However these systems can suffer from malfunctions. This is often taken into account when designing rockets. Rubber bumpers, Crumple zones, and safe launch practices can be utilized to minimize damage or injury caused by a falling rocket.

Another possible recovery system involves simply using the rocket's fins to slow its descent and is sometimes called backward sliding. By increasing fin size, more drag is generated. If the centre of mass is placed forward of the fins, the rocket will nose dive. In the case of super-roc or back-gliding rockets, the rocket is designed such that the relationship between centre of gravity and the centre of pressure of the empty rocket causes the fin-induced tendency of the rocket to tip nose down to be counteracted by the air resistance of the long body which would cause it to fall tail down, and resulting in the rocket falling sideways, slowly.[8]

Launch tubes

Some water rocket launchers use launch tubes. A launch tube fits inside the nozzle of the rocket and extends upward toward the nose. The launch tube is anchored to the ground. As the rocket begins accelerating upward, the launch tube blocks the nozzle, and very little water is ejected until the rocket leaves the launch tube. This allows almost perfectly efficient conversion of the potential energy in the compressed air to kinetic energy and gravitational potential energy of the rocket and water. The high efficiency during the initial phase of the launch is important, because rocket engines are least efficient at low speeds. A launch tube therefore significantly increases the speed and height attained by the rocket. Launch tubes are most effective when used with long rockets, which can accommodate long launch tubes.

Safety

Water rockets employ considerable amounts of energy and can be dangerous if handled improperly or in cases of faulty construction or material failure. Certain safety procedures are observed by experienced water rocket enthusiasts:

Predicting peak height

If aerodynamic drag and transient changes in pressure are neglected, a closed-form approximation for the peak height of a rocket fired vertically can be expressed as follows:

[9]

( = peak height reached, = Initial mass of water only, = Rocket mass with water, = Initial gauge pressure inside rocket, = density of water, = acceleration due to gravity) Assumptions for the above equation: (1) water is incompressible, (2) flow through the nozzle is uniform, (3) velocities are rectilinear, (4) density of water is much greater than density of air, (5) no viscosity effects, (6) steady flow, (7) velocity of the free surface of water is very small compared to the velocity of the nozzle, (8) air pressure remains constant until water runs out, (9) nozzle velocity remains constant until water runs out, and (10) there are no viscous-friction effects from the nozzle (see Moody chart).

An independent variable that influences peak height is weight/mass. Depending on the thrust of the rocket propulsion system, a rocket requires a minimum mass to overcome the deleterious effects of drag. For example, the greater the thrust/the less the original weight of the rocket, the more weight or mass must be added to the rocket to insure maximum apogee. The mass is generally referred to as ballast. This principle is demonstrated by having a student throw a straw with and without a piece of clay attached to the 'nose' of the straw. The straw with the greater mass will travel further, provided that there is sufficient thrust to overcome the ballast or extra mass.

Competitions

The Water Rocket Achievement World Record Association[10] is a worldwide association which administrates competitions for altitude records involving single-stage and multiple-stage water rockets, a flight duration competition, and speed or distance competitions for water rocket–powered cars.

Many local competitions of various sorts are held, including:

World record

Apogee photograph taken by the onboard video camera from U.S. Water Rockets' record breaking X-12 Water Rocket at an altitude of 2,068 feet (630 m).

The Guinness World Record of launching most water rockets is in hands of Kung Yik She Secondary School[25] when on 7 December 2013, they launched 1056 of them at the same time, together with primary school students in Tin Shui Wai, Hong Kong.[26]

The current record for greatest altitude achieved by a water and air propelled rocket[27] is 2723 feet (830 meters), held by the University of Cape Town[28] which achieved the feat on 26 August 2015, beating the previous record of 2044 feet (623 meters) held by US Water Rockets.[29] The rocket also carried a video camera as payload as part of the verification required by the competition rules.

Hot water rockets

Main article: Steam rocket

A steam rocket, or "hot water rocket", is a very different device - a rocket that uses water held in a pressure vessel at a high temperature, and which generates thrust through this being released as steam through a rocket nozzle.[30]

Bibliography

References

  1. Water Rocket Computer Model from NASA
  2. Sim Water Rocket from Dean's Benchtop
  3. Water Rocket Simulation from Clifford Heath's website
  4. "The 'Crushing Sleeve' Staging Mechanism ", stemharmony.com
  5. Dean's benchtop: hydrogen powered water rocket
  6. Hydroflite: Rocket Science
  7. "Super Roc Rocket Gliders", 2002, LUNAR.org
  8. Schultz, William W. "ME 495 Winter 2012 Lecture." University of Michigan, Ann Arbor. Mar.-Apr. 2012. Lecture.
  9. Water Rocket Achievement World Record Association
  10. Annual International Rocket Week
  11. STAAR Research
  12. ASTRA
  13. National Physical Laboratory's annual Water Rocket Challenge
  14. Playlist
  15. Freestyle-Physics Water Rocket Competition
  16. Rangliste Wasserraketen
  17. https://www.soinc.org/sample_k6_events#water
  18. Oleksandr, Zahoruiko. "Фестиваль "Еко-техно-Патріо" E". ueeu.in.ua.
  19. Александр, Загоруйко. "Центр інноваційних технологій освіти". ueeu.in.ua.
  20. Олександр, Загоруйко. "Робимо ракети, озброєного робота та ліс Еко-дерев". ueeu.in.ua.
  21. Олександр, Загоруйко. "Програма "ТЕРИТОРІЯ ІННОВАЦІЙ"". ueeu.in.ua.
  22. >Юные техники
  23. http://www.guinnessworldrecords.com/world-records/7000/most-water-rockets-launched-simultaneously
  24. http://www.sphrc.edu.hk/birthday.htm
  25. Single stage water rocket altitude record competition rules
  26. U.S. Water Rockets
  27. tecaeromex- steam rockets
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