Electrodynamic Combustion Control for Rocket Engines

In summary: By improving powerplant efficiency by up to 30%, this technology could also potentially be applied to rocket engines, allowing for a hybrid solution that combines the benefits of both ion propulsion and combustion rockets. Additionally, it could potentially be used to create reusable launch vehicles that are more durable and have reduced thermal stress on engine parts. Further research is needed to fully explore the possibilities and potential of Electrodynamic Combustion Control in the aerospace industry. In summary, ClearSign's technology of using electric fields to shape combustion flames shows promise in improving powerplant efficiency and has the potential to be adapted for use in rocket engines, creating a hybrid solution and potentially benefiting reusable launch vehicles.
  • #1
sanman
745
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A company called ClearSign says it can use electric fields to shape combustion flames to improve powerplant efficiency by upto 30%:

http://www.technologyreview.com/news/520466/flame-shaping-electric-fields-could-make-power-plants-cleaner/

http://www.treehugger.com/energy-ef...wer-plants-burn-cleaner-more-efficiently.htmlWhat I'd like to know is whether this approach could be used to improve rocket engine efficiency.

For instance, we know that ion propulsion engines provide higher Isp at the cost of lower thrust, which is still quite useful in low-gravity environments where high thrust isn't necessary.
But meanwhile in the Earth's gravity field, where high thrust is a necessity, we're stuck having to depend upon combustion rockets with their lower Isp.

Is it possible that Electrodynamic Combustion Control could allow us to mate ion propulsion and combustion rockets into a hybrid solution?

VASIMR is famous for allowing flexible tradeoff between Isp and thrust, but requires an unwieldy power source like nuclear or very large solar array. Meanwhile, a conventional combustion rocket produces a large amount of waste heat which might potentially be captured and recycled as electrical energy. Perhaps this could then be used to power electric fields used in Electrodynamic Combustion Control.

Clearly, a conventional rocket has a high power combustion reaction which would likely require a very large electrical field to meaningfully influence it. But ClearSign says their approach requires only a tenth of a percent of a powerplant's combustion energy to work - would that similarly be the case for a rocket engine, too?

If Electrodynamic Combustion Control can indeed work in powerplants, then does adapting it for use in a rocket engine represent a scalability problem? Could ECC be effectively used to improve rocket engine efficiency? Could it perhaps also further be used to create a hybrid rocket utilizing both chemical and ion propulsion? Could ECC be used to benefit reusable launch vehicles by reducing hotspots and associated thermal stress on engine parts, thereby increasing their longevity?
 
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  • #2
These are all questions that require further research and experimentation to answer. However, the concept of using electric fields to shape combustion flames is intriguing and could potentially be a great benefit to the aerospace industry.
 

1. What is Electrodynamic Combustion Control (ECC) for Rocket Engines?

Electrodynamic Combustion Control (ECC) for Rocket Engines is a technology that uses electrical currents to manipulate the combustion process in rocket engines. It involves placing electrodes around the combustion chamber and using them to generate electromagnetic fields that can enhance or suppress combustion reactions.

2. How does ECC improve rocket engine performance?

ECC can improve rocket engine performance by increasing the efficiency of the combustion process. By controlling the combustion reactions, ECC can optimize the fuel-air mixture and promote a more complete and stable burn. This can result in higher thrust, better fuel consumption, and reduced engine vibrations.

3. What are the potential applications of ECC in rocket propulsion?

ECC has the potential to be used in a variety of rocket propulsion systems, including liquid, solid, and hybrid rocket engines. It can also be applied to different types of fuels, such as kerosene, liquid hydrogen, and solid propellants. Additionally, ECC can be used in both small and large rocket engines, making it a versatile technology for various space missions.

4. Are there any challenges or limitations of ECC for rocket engines?

One of the main challenges of ECC is the complexity of designing and implementing the technology in rocket engines. It requires precise control of the electromagnetic fields, which can be difficult to achieve in the harsh environment of a rocket engine. Additionally, ECC may also add weight and complexity to the engine, which can be a concern for certain space missions.

5. What are the potential benefits of using ECC in rocket engines?

The potential benefits of using ECC in rocket engines include improved engine performance, greater fuel efficiency, and reduced emissions. ECC can also help increase the reliability and lifespan of rocket engines by reducing the risk of engine failures due to combustion instability. Additionally, ECC can enable more precise control of the engine, allowing for more precise trajectory and maneuvering capabilities in space missions.

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