Incident shock waves in pure CO have been characterized in the Electric Arc Shock Tube facility at NASA Ames Research Center. Spectrally and spatially resolved emission spectra characterize radiative signatures from CO in the VUV (Vacuum Ultra-Violet) and mid-infrared and atomic carbon and C2 in the visible. CO absorption of a single vibrational line is also measured with a tunable diode laser. The experimental data analyzed here are at a pressure of 0.25 Torr in the driven section and span a shock velocity range from 3.4-9.5 km/s. The emission and absorption signals are analyzed to extract temperature relaxation behind the shock which is used to derive the rate of CO dissociation. The emission spectra are compared to results using differen...
Unsteady generation of entropy and transfer of heat and chemical species in the transient oxy-combus...
The ability to control self-pressurization in cryogenic storage tanks is essential for NASAs long-te...
The uncertainty in jet energy scale is one of the dominating systematic errors for many measurements...
Use of a Sabatier reactor to recover the oxygen from the carbon dioxide exhaled by the crew on the I...
The aim of this work is to analyze a flow around the axisymmetric blunt body taken into account the ...
The hydroxyl radical (OH) fuels tropospheric ozone production and governs the lifetime of methane an...
Due to the scarcity of O_2 in the modern Martian atmosphere, Mars has been assumed to be incapable o...
A double-pulsed, 2-micron Integrated Path Differential Absorption (IPDA) lidar instrument for atmosp...
Data from test series in the Electric Arc Shock Tube Facility were previously reportedfor velocities...
The study of global warming needs precisely and accurately measuring greenhouse gases concentrations...
The purpose of this work is to develop a dynamic version of Paschen's Law that takes into account th...
Mars ISRU converts atmospheric CO2 to generate O2 and CH4. Reduces launch mass, thus mission cost. I...
While developing the aerodynamic database for the Orion spacecraft, the low-speed flight regime (tra...
The goal of a FIREMEN funded contract is the definition of a laboratory test method ranking airplane...
Transient combustion of a single biomass particle in preheated oxygen and nitrogen atmospheres with ...
Unsteady generation of entropy and transfer of heat and chemical species in the transient oxy-combus...
The ability to control self-pressurization in cryogenic storage tanks is essential for NASAs long-te...
The uncertainty in jet energy scale is one of the dominating systematic errors for many measurements...
Use of a Sabatier reactor to recover the oxygen from the carbon dioxide exhaled by the crew on the I...
The aim of this work is to analyze a flow around the axisymmetric blunt body taken into account the ...
The hydroxyl radical (OH) fuels tropospheric ozone production and governs the lifetime of methane an...
Due to the scarcity of O_2 in the modern Martian atmosphere, Mars has been assumed to be incapable o...
A double-pulsed, 2-micron Integrated Path Differential Absorption (IPDA) lidar instrument for atmosp...
Data from test series in the Electric Arc Shock Tube Facility were previously reportedfor velocities...
The study of global warming needs precisely and accurately measuring greenhouse gases concentrations...
The purpose of this work is to develop a dynamic version of Paschen's Law that takes into account th...
Mars ISRU converts atmospheric CO2 to generate O2 and CH4. Reduces launch mass, thus mission cost. I...
While developing the aerodynamic database for the Orion spacecraft, the low-speed flight regime (tra...
The goal of a FIREMEN funded contract is the definition of a laboratory test method ranking airplane...
Transient combustion of a single biomass particle in preheated oxygen and nitrogen atmospheres with ...
Unsteady generation of entropy and transfer of heat and chemical species in the transient oxy-combus...
The ability to control self-pressurization in cryogenic storage tanks is essential for NASAs long-te...
The uncertainty in jet energy scale is one of the dominating systematic errors for many measurements...