Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets

Landon T. Kamps, Yuji Saito, Ryosuke Kawabata, +4

Journal of Propulsion and Power

Nozzle-throat Reconstruction TechniqueEngineeringProfile ModificationAerospace EngineeringFluid Mechanics +11

Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using Oxygen/High-Density Polyethylene

Landon T. Kamps, Shota Hirai, Kazuhito Sakurai, +7

Journal of Propulsion and Power

Materials ScienceEngineeringReconstruction TechniqueAerospace EngineeringMechanics +10

Hybrid Rockets as Post-Boost Stages and Kick Motors

Landon T. Kamps, Shota Hirai, Harunori Nagata

Aerospace

EngineeringProfile ModificationAerospace EngineeringN2o MotorMechatronics +9

Numerical Analysis of Nozzle Erosion in Hybrid Rockets and Comparison with Experiments

Daniele Bianchi, Mario Tindaro Migliorino, Marco Rotondi, +2

Journal of Propulsion and Power

Numerical AnalysisEngineeringFluid MechanicsMechanical EngineeringGraphite Nozzle Erosion +15

Large-Scale CAMUI Type Hybrid Rocket Motor Scaling, Modeling, and Test Results

Tor Viscor, Landon T. Kamps, Kazuo Yonekura, +2

Aerospace

EngineeringRecent 40Aerospace EngineeringMechanical EngineeringMechatronics +11

The Accuracy of Reconstruction Techniques for Determining Hybrid Rocket Fuel Regression Rate

Yuji Saito, Landon T. Kamps, Kodai Komizu, +3

2018 Joint Propulsion Conference

Comprehensive Data Reduction for N2O/HDPE Hybrid Rocket Motor Performance Evaluation

Landon T. Kamps, Kazuhito Sakurai, Yuji Saito, +1

Aerospace

EngineeringFluid MechanicsMechanical EngineeringStatic Firing TestsCombustion Engineering +14

Prediction of the fuel regression-rate in a HDPE single port hybrid rocket fed by liquid nitrous oxide

Giuseppe Gallo, Landon T. Kamps, Shota Hirai, +2

Combustion and Flame

EngineeringAerospace EngineeringCombustion ScienceFuture FuelFuel Science +4

Experimental investigation of regenerative cooling performance in hybrid rocket engines

Giuseppe Gallo, Hiroki Kojima, Landon T. Kamps, +1

Thermal Science and Engineering Progress

EngineeringRocket EngineThermal ManagementHybrid Rocket EnginesThermodynamics +3

Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rocket Using Nitrous Oxide

Ryota Okuda, Kodai Komizu, Ayumu Tsuji, +6

Journal of Propulsion and Power

Chemical EngineeringNitrous OxideEngineeringAerospace EngineeringCombustion Science +11