A method of determining combustion gas flow [PDF]
, 1968 Zirconium oxide coating enables the determination of hot gas flow patterns on liquid rocket injector face and baffle surfaces to indicate modifications that will increase performance and improve combustion stability.
Bon Tempi, P. J.
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A comparison of analytical results for 20 K LOX/hydrogen instabilities [PDF]
Test data from NASA Lewis' Effect of Thrust Per Element on Combustion Stability Characteristics of Hydrogen-Oxygen Rocket Engines test program are used to validate two recently released stability analysis tools.
Breisacher, Kevin J., Klem, Mark D.
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Impact of Selected Metal Oxides on the Thermodynamics of Solid Rocket Propellant Combustion. [PDF]
MoleculesJanowska K +6 more
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JANNAF liquid rocket combustion instability panel research recommendations [PDF]
The Joint Army, Navy, NASA, Air Force (JANNAF) Liquid Rocket Combustion Instability Panel was formed in 1988, drawing its members from industry, academia, and government experts.
Klem, Mark D.
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Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]
Polymers (Basel)Chmielarek M +2 more
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Effect of model selection on combustor performance and stability predictions using ROCCID [PDF]
The ROCket Combustor Interactive Design (ROCCID) methodology is an interactive computer program that combines previously developed combustion analysis models to calculate the combustion performance and stability of liquid rocket engines.
Giuliani, James E., Klem, Mark D.
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Acute toxicity of TNT derivatives and hydrazine-based compounds from explosive and rocket fuel contamination to darkling beetles (<i>Tenebrio molitor</i> and <i>Opatrum sabulosum</i>). [PDF]
PeerJRybalka DF, Brygadyrenko VV.
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An investigation of spherical blast waves and detonation waves in a rocket combustion chamber [PDF]
Spherical blast waves and detonation waves in rocket combustion ...
Bonnell, J. M.
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Advanced Nanomaterials and Energetic Application: Experiment and Simulation. [PDF]
Nanomaterials (Basel)Pang W, Trache D, Zhang K.
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Evaluation of Proposed Rocket Engines for Earth-to-Orbit Vehicles [PDF]
The objective is to evaluate recently analyzed rocket engines for advanced Earth-to-orbit vehicles. The engines evaluated are full-flow staged combustion engines and split expander engines, both at mixture ratios at 6 and above with oxygen and hydrogen ...
Kramer, Richard D., Martin, James A.
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