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Verification of Flight Ready Hybrid Rocket Motor

Verification of Flight Ready Hybrid Rocket Motor . Presenter: Ryan Stoner Partner: Deyzi Ixtabalan Arizona State Univeristy. Objectives . Project Goals Design Fabrication Initial Testing Future Improvements . Project Goals. Identify Design Requirements.

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Verification of Flight Ready Hybrid Rocket Motor

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  1. Verification of Flight Ready Hybrid Rocket Motor Presenter: Ryan Stoner Partner: DeyziIxtabalan Arizona State Univeristy

  2. Objectives • Project Goals • Design • Fabrication • Initial Testing • Future Improvements

  3. Project Goals Identify Design Requirements • Produce an average thrust of 300lbf • Ten second burn time • Develop hybrid subsystems to accomplish steady thrust Conceptual Design Development Structural Design Cold Flow Testing Hot Fire Testing Flight Test

  4. Design of Motor

  5. Fabrication • All components were machined at the student machine shop • Both the mill and lathe were used

  6. Fabrication • Finite Element Analysis was used to verify that the parts would withstand the forces that would be applied

  7. Initial Testing Tank Pressure During Cold Flow Test

  8. Future Improvement • Replace the pyrotechnic valve with a solenoid valve • Connecting a timer to oxidizer valve • Implementing a piston in the oxidizer valve

  9. Acknowledgements • Mentor: Matt Summers • Institution: ASU/NASA Space Grant Special Thanks to:

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