An instrumentation system was developed to measure the opacity of a hybrid rocket plume as a function of optical wavelength. The source consisted of collineated beams from two lasers, providing seven wavelengths in a single probe beam. Detection was accomplished with a spec-trograph equipped with a photodiode array. Previous work with a two-wavelength system demonstrated the ability to follow the changes in opacity level of a hybrid rocket plume during the various stages of a typical firing cycle. The present work was to investigate the feasibility of using a multiple wavelength system to acquire more detailed information about the particulates present in the hybrid rocket plume. Qualitative analysis of the plume particulates was done by co...
A new multiparametric lidar system spanning from UV to mid IR is presently under testing. The system...
A new multiparametric lidar system spanning from UV to mid IR is presently under testing. The system...
The measurement of soot particulates densities in gas turbine engine and rocket exhausts is an area ...
An ideal rocket engine sensing system might probe several key elements of the rocket engine includi...
The signatures (i.e., the emission and transmission characteristics of the plumes) of various types ...
A survey was made of the spectral emissions from a 2 x 10 inch labscale hybrid rocket motor system. ...
Results from proof-of-concept tests using fiber-optic cables inserted into the combustion port of a ...
A method for in-situ optical measurements of solid and hybrid propellant rocket plumes is developed,...
The spectroscopic analysis of plume emissions is a non-intrusive method which has been used to check...
Small, portable ultraviolet and visible spectrometers can be used to characterize the combustion and...
The Optical Plume Anomaly Detection Program, an experimental study in the attempt to create a rocket...
Interest in accurate detection and targeting of aggressor missiles has received considerable interes...
This paper presents the results of an analytical study of a lidar system which uses tunable organic ...
Using a 10 N thruster engine of a LunarLander application developed by Airbus Defence & Space® and a...
A new multiparametric lidar system spanning from UV to mid IR is presently under testing. The system...
A new multiparametric lidar system spanning from UV to mid IR is presently under testing. The system...
A new multiparametric lidar system spanning from UV to mid IR is presently under testing. The system...
The measurement of soot particulates densities in gas turbine engine and rocket exhausts is an area ...
An ideal rocket engine sensing system might probe several key elements of the rocket engine includi...
The signatures (i.e., the emission and transmission characteristics of the plumes) of various types ...
A survey was made of the spectral emissions from a 2 x 10 inch labscale hybrid rocket motor system. ...
Results from proof-of-concept tests using fiber-optic cables inserted into the combustion port of a ...
A method for in-situ optical measurements of solid and hybrid propellant rocket plumes is developed,...
The spectroscopic analysis of plume emissions is a non-intrusive method which has been used to check...
Small, portable ultraviolet and visible spectrometers can be used to characterize the combustion and...
The Optical Plume Anomaly Detection Program, an experimental study in the attempt to create a rocket...
Interest in accurate detection and targeting of aggressor missiles has received considerable interes...
This paper presents the results of an analytical study of a lidar system which uses tunable organic ...
Using a 10 N thruster engine of a LunarLander application developed by Airbus Defence & Space® and a...
A new multiparametric lidar system spanning from UV to mid IR is presently under testing. The system...
A new multiparametric lidar system spanning from UV to mid IR is presently under testing. The system...
A new multiparametric lidar system spanning from UV to mid IR is presently under testing. The system...
The measurement of soot particulates densities in gas turbine engine and rocket exhausts is an area ...