Verification of Flight Ready Hybrid Rocket Motor

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Verification of Flight Ready Hybrid Rocket Motor Presenter: Ryan Stoner Partner: Deyzi Ixtabalan Arizona State Univeristy

description

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. - PowerPoint PPT Presentation

Transcript of Verification of Flight Ready Hybrid Rocket Motor

Page 1: Verification of Flight Ready Hybrid Rocket Motor

Verification of Flight Ready Hybrid Rocket Motor

Presenter:Ryan Stoner

Partner:Deyzi Ixtabalan

Arizona State Univeristy

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Objectives

Project GoalsDesignFabricationInitial TestingFuture Improvements

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Project GoalsProduce an average

thrust of 300lbf

Ten second burn time

Develop hybrid subsystems to accomplish steady thrust

Identify Design

RequirementsConceptual

Design Development

Structural Design

Cold Flow Testing

Hot Fire Testing

Flight Test

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Design of Motor

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FabricationAll components were

machined at the student machine shop

• Both the mill and lathe were used

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Fabrication

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

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Initial Testing

Tank Pressure During Cold Flow Test

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Future Improvement Replace the pyrotechnic

valve with a solenoid valve

Connecting a timer to oxidizer valve

Implementing a piston in the oxidizer valve

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Acknowledgements

Mentor: Matt SummersInstitution: ASU/NASA Space Grant

Special Thanks to: