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What is the job of the acoustic cavities inside the main combustion chamber?


How does a launch vehicle control its trajectory during the first stage?How will the SLS first stage be supplied with engines? Copy manufacturing the RS-25 or replacing it?How is a rocket engine started?Limiting factors of liquid rocket engine thrustWhat are the two very large “blue” cylinders attaching to the combustion chamber of each Rutherford Engine?F1 engine specification?What's the actual oxidizer/fuel ratio in the combustion chamber of the Vulcain?How to measure the temperature inside a combustion chamberHow much fuel/oxidizer was held in the piping of the Shuttle orbiter?What Constitutes A Combustion Chamber?






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6












$begingroup$


I am new to rocket engines. I was looking at an image of RS-25 engine's MCC and found these acoustic cavities, and I want to know how they work. Can somebody please explain their working principle? Thank you. the image










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    6












    $begingroup$


    I am new to rocket engines. I was looking at an image of RS-25 engine's MCC and found these acoustic cavities, and I want to know how they work. Can somebody please explain their working principle? Thank you. the image










    share|improve this question









    New contributor



    Aungmyintmyat Hane is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
    Check out our Code of Conduct.






    $endgroup$














      6












      6








      6





      $begingroup$


      I am new to rocket engines. I was looking at an image of RS-25 engine's MCC and found these acoustic cavities, and I want to know how they work. Can somebody please explain their working principle? Thank you. the image










      share|improve this question









      New contributor



      Aungmyintmyat Hane is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.






      $endgroup$




      I am new to rocket engines. I was looking at an image of RS-25 engine's MCC and found these acoustic cavities, and I want to know how they work. Can somebody please explain their working principle? Thank you. the image







      space-shuttle engines engine-design ssme combustion-chamber






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      edited 10 hours ago







      Aungmyintmyat Hane













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          1 Answer
          1






          active

          oldest

          votes


















          8












          $begingroup$

          They are provided to help damp out combustion instabilities.




          The main injector uses cooled baffle elements, developed at Glenn in
          the 1960s to control pressure waves that could destroy the engine.
          Pressure waves in the space shuttle main engine combustion chamber are
          also controlled by acoustic cavities. Testing by Glenn engineers
          determined the most effective size and location of these cavities,
          which act somewhat like cavities in acoustic ceilings.




          Source



          You can read more on the theory of how they work in this book Liquid Rocket Engine Combustion Instability starting at page 384.



          It starts out




          Acoustic cavities such as Helmholtz and quarter-wave resonators were
          successfully used as damping devices for the suppression of
          combustion oscillations. resonator consists of a small volume
          connected with the combustion chamber through an orifice. If the
          dimensions of the various resonator elements are small in comparison
          to the wavelength of the oscillation, the gas motion behavior in the
          resonator is analogous to a mass-spring-dashpot system.




          Acoustic cavity design is also discussed in the NASA monograph Liquid Rocket Engine Combustion Stabilization Devices. It includes this figure showing some other applications.



          enter image description here






          share|improve this answer











          $endgroup$















            Your Answer








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            1 Answer
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            1 Answer
            1






            active

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            votes









            active

            oldest

            votes






            active

            oldest

            votes









            8












            $begingroup$

            They are provided to help damp out combustion instabilities.




            The main injector uses cooled baffle elements, developed at Glenn in
            the 1960s to control pressure waves that could destroy the engine.
            Pressure waves in the space shuttle main engine combustion chamber are
            also controlled by acoustic cavities. Testing by Glenn engineers
            determined the most effective size and location of these cavities,
            which act somewhat like cavities in acoustic ceilings.




            Source



            You can read more on the theory of how they work in this book Liquid Rocket Engine Combustion Instability starting at page 384.



            It starts out




            Acoustic cavities such as Helmholtz and quarter-wave resonators were
            successfully used as damping devices for the suppression of
            combustion oscillations. resonator consists of a small volume
            connected with the combustion chamber through an orifice. If the
            dimensions of the various resonator elements are small in comparison
            to the wavelength of the oscillation, the gas motion behavior in the
            resonator is analogous to a mass-spring-dashpot system.




            Acoustic cavity design is also discussed in the NASA monograph Liquid Rocket Engine Combustion Stabilization Devices. It includes this figure showing some other applications.



            enter image description here






            share|improve this answer











            $endgroup$

















              8












              $begingroup$

              They are provided to help damp out combustion instabilities.




              The main injector uses cooled baffle elements, developed at Glenn in
              the 1960s to control pressure waves that could destroy the engine.
              Pressure waves in the space shuttle main engine combustion chamber are
              also controlled by acoustic cavities. Testing by Glenn engineers
              determined the most effective size and location of these cavities,
              which act somewhat like cavities in acoustic ceilings.




              Source



              You can read more on the theory of how they work in this book Liquid Rocket Engine Combustion Instability starting at page 384.



              It starts out




              Acoustic cavities such as Helmholtz and quarter-wave resonators were
              successfully used as damping devices for the suppression of
              combustion oscillations. resonator consists of a small volume
              connected with the combustion chamber through an orifice. If the
              dimensions of the various resonator elements are small in comparison
              to the wavelength of the oscillation, the gas motion behavior in the
              resonator is analogous to a mass-spring-dashpot system.




              Acoustic cavity design is also discussed in the NASA monograph Liquid Rocket Engine Combustion Stabilization Devices. It includes this figure showing some other applications.



              enter image description here






              share|improve this answer











              $endgroup$















                8












                8








                8





                $begingroup$

                They are provided to help damp out combustion instabilities.




                The main injector uses cooled baffle elements, developed at Glenn in
                the 1960s to control pressure waves that could destroy the engine.
                Pressure waves in the space shuttle main engine combustion chamber are
                also controlled by acoustic cavities. Testing by Glenn engineers
                determined the most effective size and location of these cavities,
                which act somewhat like cavities in acoustic ceilings.




                Source



                You can read more on the theory of how they work in this book Liquid Rocket Engine Combustion Instability starting at page 384.



                It starts out




                Acoustic cavities such as Helmholtz and quarter-wave resonators were
                successfully used as damping devices for the suppression of
                combustion oscillations. resonator consists of a small volume
                connected with the combustion chamber through an orifice. If the
                dimensions of the various resonator elements are small in comparison
                to the wavelength of the oscillation, the gas motion behavior in the
                resonator is analogous to a mass-spring-dashpot system.




                Acoustic cavity design is also discussed in the NASA monograph Liquid Rocket Engine Combustion Stabilization Devices. It includes this figure showing some other applications.



                enter image description here






                share|improve this answer











                $endgroup$



                They are provided to help damp out combustion instabilities.




                The main injector uses cooled baffle elements, developed at Glenn in
                the 1960s to control pressure waves that could destroy the engine.
                Pressure waves in the space shuttle main engine combustion chamber are
                also controlled by acoustic cavities. Testing by Glenn engineers
                determined the most effective size and location of these cavities,
                which act somewhat like cavities in acoustic ceilings.




                Source



                You can read more on the theory of how they work in this book Liquid Rocket Engine Combustion Instability starting at page 384.



                It starts out




                Acoustic cavities such as Helmholtz and quarter-wave resonators were
                successfully used as damping devices for the suppression of
                combustion oscillations. resonator consists of a small volume
                connected with the combustion chamber through an orifice. If the
                dimensions of the various resonator elements are small in comparison
                to the wavelength of the oscillation, the gas motion behavior in the
                resonator is analogous to a mass-spring-dashpot system.




                Acoustic cavity design is also discussed in the NASA monograph Liquid Rocket Engine Combustion Stabilization Devices. It includes this figure showing some other applications.



                enter image description here







                share|improve this answer














                share|improve this answer



                share|improve this answer








                edited 9 hours ago

























                answered 10 hours ago









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