Flight Test Demonstration Of Led-Based Fire Sensors For Space Propulsion Vehicles
Keywords
Crew health monitoring; Fire detection; Primary life support; Space systems
Abstract
Gases which are indicative of combustion and pyrolysis have absorption features in the mid-infrared range. Therefore, it is possible to implement absorption spectroscopy as a detection method to provide real time monitoring of gases in spacecraft. A sensor developed at the University of Central Florida for this purpose was flown on a proof of concept test flight through partnerships with NASA's Columbia Scientific Balloon Facility (CSBF) and the Louisiana State University (LSU) High Altitude Student Payload (HASP). The test flight enabled autonomous operation of the sensor at an altitude of 105,000ft (32km). The sensor utilizes a 4.2 μm light-emitting diode (LED) source, amplitude modulation to characterize CO2 concentration, and frequency modulation to characterize ambient temperature.
Publication Date
1-1-2018
Publication Title
2018 Spring Technical Meeting of the Eastern States Section of the Combustion Institute, ESSCI 2018
Volume
2018-March
Document Type
Article; Proceedings Paper
Personal Identifier
scopus
Copyright Status
Unknown
Socpus ID
85048961184 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/85048961184
STARS Citation
Terracciano, Anthony Carmine; Thurmond, Kyle; Villar, Michael; Urso, Justin; and Ninnemann, Erik, "Flight Test Demonstration Of Led-Based Fire Sensors For Space Propulsion Vehicles" (2018). Scopus Export 2015-2019. 8086.
https://stars.library.ucf.edu/scopus2015/8086