Inverse Hybrid Rocket report

Inverse Hybrid Rocket report - InverseHybridRocketProject...

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    Inverse Hybrid Rocket Project Adam Irvine Scott Bishop
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Introduction Solid Motor Advantages Simple Heritage Disadvantages Lower Isp No Throttle  Control Small Cracks  Can Lead To  Failure Liquid Motor Advantages Highest Isp Throttle Control Disadvantages Higher Weight Of  Inert Mass Complex Lower Propellant  Density Hybrid Motor Advantages Higher Isp Than  Solids Throttle Control Simple Robust Large Number Of  Propellants To  Chose From Disadvantages Low Bulk Density
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Introduction      General Isp  Comparison Hybrid History First Hybrid  Program In 1930s Largely  Unsuccessful Due  To Choice Of Fuel Successful Program  Started In 40s Mid 50s G. Moore And K.  Berman W. Avery Liquid 320-460 Solid 260-300 Hybrid 290-350
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Introduction Low Liquid To Solid Ratio Could Lead To  Hybrids With Higher Bulk Density High Enough Benefit Could Offset Low  Performance No Data Could Be Found Tests Will Have To Be Conducted
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Outline Goal Is To Launch Inverse Hybrid Motor Theoretical Performance Calculated Test Conducted To Verify Performance Construct Final Motor Build Rocket To Fit Motor Analyze Results
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Design Components Fuel Tank Injector Pyrovalve Nozzle Fill Port Constraints Thrust: 100lbs Chamber Pressure: 100psi Diameter:  2in Chemicals Used: ApSi and Methanol
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Design Burn Rate Was Needed For  NASA Code The NASA Thermochemisty 
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This note was uploaded on 01/15/2012 for the course AAE 490 taught by Professor Andrisani during the Fall '09 term at Purdue University-West Lafayette.

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Inverse Hybrid Rocket report - InverseHybridRocketProject...

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