Departures from Ideal Performance
Thrust Nozzle Optimization Including Boundary-Layer Effects
Hybrid Rocket Motor
University of Pennsylvania Hybrid Rocket Homepage
Variable Valve Hybrid Rocket Motor Proposal
Variable Valve Hybrid Rocket Motor Report 1
Solid Propellant Rocket Motor Design and Testing
Solid Rocket Motor Performance Analysis and Prediction
Solid Propellant Grain Design and Internal Ballistics
RPE HYBRID PROPELLANT ROCKETS
Regression Rate Behavior of Hybrid Rocket Solid Fuels
Development Work on a Small Experimental Hybrid Rocket
Hybrid Rocket Motor webpage by Fintel
Development of a Reusable Aerospike Nozzle for Hybrid Rocket Motors
Fuel Regression Rate Characterization Using a Laboratory Scale Notrous Oxide Hybrid Propulsion System
Testing of Paraffin-Based Hybrid Rocket Fuel Using Hydrogen Peroxide Oxidizer
NITROUS OXIDE HYBRID ROCKET FUEL PERFORMANCE AND STABILITY
Hybrid Rocket Motor
Using the Mel-Temp Apparatus
Method for Measuring Thermal Conductivity of Small Samples Having Very Low Thermal Conductivity
Primer on Pressure Transducers
Another Transducer Primer
General Spec Sheet for Taber Pressure Transducer
Taber Transducer Spec Sheet
Development and Launch of the Purdue Hybrid Rocket Technology Demonstrator
I am Samuel "Red" Otto. This blog documents my progress on projects in propulsion and CFD. In Research Science with Graig Marx, my focus is on the regression behavior of liquefying hybrid rocket fuels, determining the dependence of regression rate coefficients on the Thermal Properties of n-paraffin fuels. In ACSI with David Nassar, I am investigating core flows in a hybrid rocket motor using a MUSCL scheme in conjunction with the Advection Upstream Splitting Method (AUSM) for flux evaluation.
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