Not listed MY RESEARCH ADDRESSES THE SOURCES OF ERROR USING UNSTEADY PRESSURE-SENSITIVE PAINT (PSP) AND THE DEVELOPMENT OF HIGH-TEMPERATURE TEMPERATURE-SENSITIVE PAINT (TSP). NASA CAN CURRENTLY USE STEADY STATE PSP WITH RELATIVE EASE; UNSTEADY PSP ON THE OTHER HAND STILL IS HINDERED BY MULTIPLE SOURCES OF ERROR. THIS IS WHAT I INTEND TO CHARACTERIZE WITH MY RESEARCH AND IN DOING SO OFFER SOLUTIONS TO REDUCE OR CORRECT FOR ERRORS FROM LIGHT AND PAINT INTENSITY DECAY PAINT THICKNESS UNEVENNESS PAINT SURFACE ROUGHNESS AND TEMPERATURE SENSITIVITY OF THE PAINT. WITH THESE CHARACTERIZATIONS I PROPOSE DEVELOPING A CALIBRATION PROCEDURE TO ALLOW UNSTEADY PSP TO BE RELIABLY USED WITHOUT THE CURRENT NECESSITY OF MANY EXPENSIVE UNSTEADY PRESSURE TRANSDUCERS TO VERIFY THE DATA. THIS WILL PROVIDE A RELIABLE GLOBAL PRESSURE SENSOR ENABLING MORE ACCURATE MEASUREMENTS OF LOADS ACTING ON AERODYNAMIC BODIES. MY RESEARCH INTO TSP IS FOCUSED ON INCREASING RESPONSE TIME THROUGH CHARACTERIZATION OF PAINTS USING DIFFERENT LUMINOPHORES (LUMINESCENT MOLECULES) THAN THOSE USED IN CURRENTLY AVAILABLE PAINTS. THROUGH THE USE OF DIFFERENT LUMINOPHORES AND BINDING MATRICES I AM ALSO INVESTIGATING THE DEVELOPMENT OF TSPS FOR TEMPERATURES IN EXCESS OF 1000K. THESE PAINTS CAN THEN BE USED FOR THE DEVELOPMENT OF HYPERSONIC VEHICLES. ($1k) 4/23/19 3 MY RESEARCH ADDRESSES THE SOURCES OF ERROR USING UNSTEADY PRESSURE-SENSITIVE PAINT (PSP) AND THE DEVELOPMENT OF HIGH-TEMPERATURE TEMPERATURE-SENSITIVE PAINT (TSP). NASA CAN CURRENTLY USE STEADY STATE PSP WITH RELATIVE EASE; UNSTEADY PSP, ON THE OTHER HAND, STILL IS HINDERED BY MULTIPLE SOURCES OF ERROR. THIS IS WHAT I INTEND TO CHARACTERIZE WITH MY RESEARCH AND IN DOING SO OFFER SOLUTIONS TO REDUCE OR CORRECT FOR ERRORS FROM LIGHT AND PAINT INTENSITY DECAY, PAINT THICKNESS UNEVENNESS, PAINT SURFACE ROUGHNESS, AND TEMPERATURE SENSITIVITY OF THE PAINT. WITH THESE CHARACTERIZATIONS, I PROPOSE DEVELOPING A CALIBRATION PROCEDURE TO ALLOW UNSTEADY PSP TO BE RELIABLY USED WITHOUT THE CURRENT NECESSITY OF MANY EXPENSIVE UNSTEADY PRESSURE TRANSDUCERS TO VERIFY THE DATA. THIS WILL PROVIDE A RELIABLE GLOBAL PRESSURE SENSOR, ENABLING MORE ACCURATE MEASUREMENTS OF LOADS ACTING ON AERODYNAMIC BODIES. MY RESEARCH INTO TSP IS FOCUSED ON INCREASING RESPONSE TIME THROUGH CHARACTERIZATION OF PAINTS USING DIFFERENT LUMINOPHORES (LUMINESCENT MOLECULES) THAN THOSE USED IN CURRENTLY AVAILABLE PAINTS. THROUGH THE USE OF DIFFERENT LUMINOPHORES AND BINDING MATRICES, I AM ALSO INVESTIGATING THE DEVELOPMENT OF TSPS FOR TEMPERATURES IN EXCESS OF 1000K. THESE PAINTS CAN THEN BE USED FOR THE DEVELOPMENT OF HYPERSONIC VEHICLES. Funding Only Action ($1k) 4/23/19 Not listed MY RESEARCH ADDRESSES THE SOURCES OF ERROR USING UNSTEADY PRESSURE-SENSITIVE PAINT (PSP) AND THE DEVELOPMENT OF HIGH-TEMPERATURE TEMPERATURE-SENSITIVE PAINT (TSP). NASA CAN CURRENTLY USE STEADY STATE PSP WITH RELATIVE EASE; UNSTEADY PSP ON THE OTHER HAND STILL IS HINDERED BY MULTIPLE SOURCES OF ERROR. THIS IS WHAT I INTEND TO CHARACTERIZE WITH MY RESEARCH AND IN DOING SO OFFER SOLUTIONS TO REDUCE OR CORRECT FOR ERRORS FROM LIGHT AND PAINT INTENSITY DECAY PAINT THICKNESS UNEVENNESS PAINT SURFACE ROUGHNESS AND TEMPERATURE SENSITIVITY OF THE PAINT. WITH THESE CHARACTERIZATIONS I PROPOSE DEVELOPING A CALIBRATION PROCEDURE TO ALLOW UNSTEADY PSP TO BE RELIABLY USED WITHOUT THE CURRENT NECESSITY OF MANY EXPENSIVE UNSTEADY PRESSURE TRANSDUCERS TO VERIFY THE DATA. THIS WILL PROVIDE A RELIABLE GLOBAL PRESSURE SENSOR ENABLING MORE ACCURATE MEASUREMENTS OF LOADS ACTING ON AERODYNAMIC BODIES. MY RESEARCH INTO TSP IS FOCUSED ON INCREASING RESPONSE TIME THROUGH CHARACTERIZATION OF PAINTS USING DIFFERENT LUMINOPHORES (LUMINESCENT MOLECULES) THAN THOSE USED IN CURRENTLY AVAILABLE PAINTS. THROUGH THE USE OF DIFFERENT LUMINOPHORES AND BINDING MATRICES I AM ALSO INVESTIGATING THE DEVELOPMENT OF TSPS FOR TEMPERATURES IN EXCESS OF 1000K. THESE PAINTS CAN THEN BE USED FOR THE DEVELOPMENT OF HYPERSONIC VEHICLES. $0 8/15/18 2 MY RESEARCH ADDRESSES THE SOURCES OF ERROR USING UNSTEADY PRESSURE-SENSITIVE PAINT (PSP) AND THE DEVELOPMENT OF HIGH-TEMPERATURE TEMPERATURE-SENSITIVE PAINT (TSP). NASA CAN CURRENTLY USE STEADY STATE PSP WITH RELATIVE EASE; UNSTEADY PSP, ON THE OTHER HAND, STILL IS HINDERED BY MULTIPLE SOURCES OF ERROR. THIS IS WHAT I INTEND TO CHARACTERIZE WITH MY RESEARCH AND IN DOING SO OFFER SOLUTIONS TO REDUCE OR CORRECT FOR ERRORS FROM LIGHT AND PAINT INTENSITY DECAY, PAINT THICKNESS UNEVENNESS, PAINT SURFACE ROUGHNESS, AND TEMPERATURE SENSITIVITY OF THE PAINT. WITH THESE CHARACTERIZATIONS, I PROPOSE DEVELOPING A CALIBRATION PROCEDURE TO ALLOW UNSTEADY PSP TO BE RELIABLY USED WITHOUT THE CURRENT NECESSITY OF MANY EXPENSIVE UNSTEADY PRESSURE TRANSDUCERS TO VERIFY THE DATA. THIS WILL PROVIDE A RELIABLE GLOBAL PRESSURE SENSOR, ENABLING MORE ACCURATE MEASUREMENTS OF LOADS ACTING ON AERODYNAMIC BODIES. MY RESEARCH INTO TSP IS FOCUSED ON INCREASING RESPONSE TIME THROUGH CHARACTERIZATION OF PAINTS USING DIFFERENT LUMINOPHORES (LUMINESCENT MOLECULES) THAN THOSE USED IN CURRENTLY AVAILABLE PAINTS. THROUGH THE USE OF DIFFERENT LUMINOPHORES AND BINDING MATRICES, I AM ALSO INVESTIGATING THE DEVELOPMENT OF TSPS FOR TEMPERATURES IN EXCESS OF 1000K. THESE PAINTS CAN THEN BE USED FOR THE DEVELOPMENT OF HYPERSONIC VEHICLES. Other Administrative Action $0 8/15/18 Not listed MY RESEARCH ADDRESSES THE SOURCES OF ERROR USING UNSTEADY PRESSURE-SENSITIVE PAINT (PSP) AND THE DEVELOPMENT OF HIGH-TEMPERATURE TEMPERATURE-SENSITIVE PAINT (TSP). NASA CAN CURRENTLY USE STEADY STATE PSP WITH RELATIVE EASE; UNSTEADY PSP ON THE OTHER HAND STILL IS HINDERED BY MULTIPLE SOURCES OF ERROR. THIS IS WHAT I INTEND TO CHARACTERIZE WITH MY RESEARCH AND IN DOING SO OFFER SOLUTIONS TO REDUCE OR CORRECT FOR ERRORS FROM LIGHT AND PAINT INTENSITY DECAY PAINT THICKNESS UNEVENNESS PAINT SURFACE ROUGHNESS AND TEMPERATURE SENSITIVITY OF THE PAINT. WITH THESE CHARACTERIZATIONS I PROPOSE DEVELOPING A CALIBRATION PROCEDURE TO ALLOW UNSTEADY PSP TO BE RELIABLY USED WITHOUT THE CURRENT NECESSITY OF MANY EXPENSIVE UNSTEADY PRESSURE TRANSDUCERS TO VERIFY THE DATA. THIS WILL PROVIDE A RELIABLE GLOBAL PRESSURE SENSOR ENABLING MORE ACCURATE MEASUREMENTS OF LOADS ACTING ON AERODYNAMIC BODIES. MY RESEARCH INTO TSP IS FOCUSED ON INCREASING RESPONSE TIME THROUGH CHARACTERIZATION OF PAINTS USING DIFFERENT LUMINOPHORES (LUMINESCENT MOLECULES) THAN THOSE USED IN CURRENTLY AVAILABLE PAINTS. THROUGH THE USE OF DIFFERENT LUMINOPHORES AND BINDING MATRICES I AM ALSO INVESTIGATING THE DEVELOPMENT OF TSPS FOR TEMPERATURES IN EXCESS OF 1000K. THESE PAINTS CAN THEN BE USED FOR THE DEVELOPMENT OF HYPERSONIC VEHICLES. $47.0k 6/12/17