WT Aerospace Engineering

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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Wednesday, September 21, 2011

Successful Static Firing of APCP motor

Posted by AerospaceNerd at 4:21 PM
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Blog Archive

  • ▼  2011 (17)
    • ▼  September (4)
      • Initial direction based off of preliminary research
      • Project Refinement #1
      • Characterization of Hybrid Rocket Propellant Regre...
      • Successful Static Firing of APCP motor
    • ►  October (6)
    • ►  November (5)
    • ►  December (2)
  • ►  2012 (14)
    • ►  January (9)
    • ►  February (3)
    • ►  March (2)
  • ►  2013 (2)
    • ►  March (2)

Research Science (Propellant Research)

  • Research Plan
  • Methods rev.2
  • Methods rev.1
  • Introduction rev.4
  • Introduction rev.3
  • Introduction rev.2
  • Introduction rev.1

Document Abstracts

  • Scale-Up Tests of High Regression Rate Liquefying Hybrid Rocket Fuels
  • Bistetrazoles: Nitrogen-Rich, High-Performing, Insensitive Energetic Compounds
  • Testing of Paraffin-Based Hybrid Rocket Fuel Using Hydrogen Peroxide Oxidizer
  • Fuel Regression Rate Characterization Using a Laboratory Scale Nitrous Oxide Hybrid Propulsion System
  • Regression Rate Behavior of Hybrid Rocket Solid Fuels
  • Energetic nitrogen-rich salts and ionic liquids: 5-aminotetrazole (AT) as a weak acid
  • DEVELOPMENT OF SCALABLE SPACE-TIME AVERAGED REGRESSION RATE EXPRESSIONS FOR HYBRID ROCKETS
  • Bis Triaminoguanidinium Azotetrazolate (TAGzT) Scale Up And Production
  • Synthesis of Insensitive 5,50-Azotetrazolate Salts
  • Hybrid Rocket Technology
  • Hydrazinium 5-Aminotetrazolate: an Insensitive Energetic Material Containing 83.72% Nitrogen
  • High Nitrogen Compounds For Use in Low-Erosivity Gun Propellants
  • Application of Ionic Liquids to Space Propulsion
  • Hybrid Rocket Motor
  • Analysis of Hydroxylammonium Nitrate Based Liquid Propellants
  • Development and Testing of Paraffin-Based Hybrid Rocket Fuels
  • Improvements in the Synthesis of Guanidinium Azotetrazolate (GuZT)
  • Synthesis, Characterization and Thermal Behavior of Hydrazinium Nitroformate (HNF) and its New N-alkyl Substituted Derivatives
  • Ammonia-Borane and Related N-B-H Compounds and Materials: Safety Aspects, Properties and applications
  • An Experimental Investigation of A Lithium Aluminum Hydride-Hydrogen Peroxide Hybrid Rocket
  • ADN-The New Oxidizer Around the Corner for an Environmentally Friendly Smokeless Propellant
  • Guanidinium Azo-Tetrazolate (GAT) as a High Performance Hybrid Rocket Fuel Additive
  • Development of Novel Polynitrogen-based High-Performance Solid Propellants
  • Advances in High Energy Materials Abstract
  • ALICE Propellant Abstract
  • Borane Performance in Turbojet Abstract
  • High Energy-Density Liquid Rocket Fuel Performance
  • Hybrid Rocket Science Abstract
  • Rocket Propulsion Elements Abstract

Advanced Computer Science and Innovations (CFD Research)

  • Rough Project Timeline
  • Introduction and Abstract
  • ACSI Annotated Bibliography
  • Research Question and Strategic Planning

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Links

  • WT-Research Science
  • Iowa Amateur Rocketry Group (IARG)
  • Hybrid Rocket Motor
  • Amateur Rocketry Links Library
  • NASA Technical Documents
  • NACA Library
  • NASA Technical Reports Server
  • NISCAIR ONLINE PERIODICALS REPOSITORY (NOPR)
  • Compressible Aerodynamics
  • RPA-Tool for Rocket Propulsion Analysis
  • Amateur Rocket Motor Chemicals & Supplies
  • Rockets "R" Us (awesome supplier)
  • Peroxide Propulsion (H2O2 supply)
  • McMaster-Carr
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