FAA, Fire Safety. This collection contains reports and resources from the Federal Aviation Administration’s Fire Safety Branch research program. Bookmark this collection: https://rosap.ntl.bts.gov/collection_fire_safety.
The aircraft industry in partnership with the Federal Aviation Administration (FAA) formed a task group in 2013 to consider using the American Society for Testing and Materials (ASTM) D7309 "Standard Test Method for Determining Flammability Characteristics of Plastics and Other Combustible Solid Materials Using Microscale Combustion Calorimetry" (M
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Lyon, R. E., Walters, R. N., Safronava, N., & Guo, H. (2022). Accounting for Baseline Drift in the Microscale Combustion Calorimeter (Report No. DOT/FAA/TC-22/31). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1524521
Lyon, Richard E., Richard N. Walters, Natallia Safronava, and Haiqing Guo. Accounting for Baseline Drift in the Microscale Combustion Calorimeter. Report no. DOT/FAA/TC-22/31. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022. https://doi.org/10.21949/1524521.
Lyon, Richard E., et al. Accounting for Baseline Drift in the Microscale Combustion Calorimeter. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022, Report no. DOT/FAA/TC-22/31, ROSA P. https://doi.org/10.21949/1524521.
A simulated model of a full-sized aircraft cargo compartment was used to determine the effect of active cargo containers. Physical testing in conjunction with the simulated cargo compartment was used to validate the accuracy of the Fire Dynamics Simulator model which included an artificial smoke generator. The artificial smoke generator is currentl
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Ferraro, A. (2022). Effect of Active Cargo Containers on Aircraft Smoke Transport (Report No. DOT/FAA/TCTT-22/30). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1524503
Ferraro, Andrew. Effect of Active Cargo Containers on Aircraft Smoke Transport. Report no. DOT/FAA/TCTT-22/30. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022. https://doi.org/10.21949/1524503.
Ferraro, Andrew Effect of Active Cargo Containers on Aircraft Smoke Transport. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022, Report no. DOT/FAA/TCTT-22/30, ROSA P. https://doi.org/10.21949/1524503.
A method and criterion are described to assess the no-effect level of a constituent change on the fire performance of aircraft cabin material or construction. A constituent may be a thermosetting resin, coating, composite, adhesive, potting compound, film, fabric, elastomer, rubber, or thermoplastic. This can be used in the construction of a cabin
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Safronava, N., & Lyon, R. E. (2022). Microscale Flammability Criterion for Constituents of Aircraft Cabin Materials (Report No. DOT/FAA/TC-22/22). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1524498
Safronava, Natallia and Richard E. Lyon. Microscale Flammability Criterion for Constituents of Aircraft Cabin Materials. Report no. DOT/FAA/TC-22/22. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022. https://doi.org/10.21949/1524498.
Safronava, Natallia, and Richard E. Lyon Microscale Flammability Criterion for Constituents of Aircraft Cabin Materials. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022, Report no. DOT/FAA/TC-22/22, ROSA P. https://doi.org/10.21949/1524498.
In February 2022, a package containing 140 lithium-ion pouch cells caught fire on a conveyor belt in a sort facility of an all-cargo airline. One of the packages in the shipment was sent to the Federal Aviation Administration's (FAA) William J. Hughes Technical Center for hazard evaluation. Specialized cell analysis equipment was used to determine
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Keslar, D. (2022). An Analysis of State of Charge in Lithium-ion Batteries (Report No. DOT/FAA/TCTN-22/27). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1524506
Keslar, Daniel. An Analysis of State of Charge in Lithium-ion Batteries. Report no. DOT/FAA/TCTN-22/27. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022. https://doi.org/10.21949/1524506.
Keslar, Daniel An Analysis of State of Charge in Lithium-ion Batteries. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022, Report no. DOT/FAA/TCTN-22/27, ROSA P. https://doi.org/10.21949/1524506.
This research seeks to support the United Nations (UN) Subcommittee of Experts on the Transport of Dangerous Goods (SCOE TDG) establish a more performance-based approach to classifying the various types of lithium-ion batteries for transportation. A proposed standardized test method was used to assess the combustion hazard from a lithium-ion batter
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Karp, M., & Sica, J. (2022). Evaluation of Lithium Battery Thermal Runaway Vent Gas Combustion (Report No. DOT/FAA/TC-22/12). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1528205
Karp, Matthew and Joseph Sica. Evaluation of Lithium Battery Thermal Runaway Vent Gas Combustion. Report no. DOT/FAA/TC-22/12. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022. https://doi.org/10.21949/1528205.
Karp, Matthew, and Joseph Sica Evaluation of Lithium Battery Thermal Runaway Vent Gas Combustion. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022, Report no. DOT/FAA/TC-22/12, ROSA P. https://doi.org/10.21949/1528205.
Although the UN classifies lithium batteries as dangerous goods, current UN numbers for lithium batteries do not indicate what level of hazard each individual shipment may pose. Lithium batteries can exhibit varied temperature rise and propagation characteristics when heated to thermal runaway. Therefore, This study was conducted to characterize th
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Maloney, T. (2022). Evaluation of Lithium Battery Thermal Runaway Propagation (Report No. DOT/FAA/TC-TN21/54). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/60114
Maloney, Thomas. Evaluation of Lithium Battery Thermal Runaway Propagation. Report no. DOT/FAA/TC-TN21/54. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022. https://rosap.ntl.bts.gov/view/dot/60114.
Maloney, Thomas Evaluation of Lithium Battery Thermal Runaway Propagation. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2022, Report no. DOT/FAA/TC-TN21/54, ROSA P. https://rosap.ntl.bts.gov/view/dot/60114.
Knowing fire temperature and soot concentration in a fire is very important in fire safety research. The fire radiant energy, a function of fire temperature and soot concentration, contributes about 40% of energy loss to the walls of the Ohio State University (OSU) fire calorimeter during the burning of large area cabin materials. This report prese
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Guo, H., & Lyon, R. E. (2021). A Digital Imaging Technique to Measure Temperatures and Soot Concentrations in Flames of Condensed Phase Fuels (Report No. DOT/FAA/TC-21/50). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/60770
Guo, Haiqing and Richard E. Lyon. A Digital Imaging Technique to Measure Temperatures and Soot Concentrations in Flames of Condensed Phase Fuels. Report no. DOT/FAA/TC-21/50. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2021. https://rosap.ntl.bts.gov/view/dot/60770.
Guo, Haiqing, and Richard E. Lyon A Digital Imaging Technique to Measure Temperatures and Soot Concentrations in Flames of Condensed Phase Fuels. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2021, Report no. DOT/FAA/TC-21/50, ROSA P. https://rosap.ntl.bts.gov/view/dot/60770.
Hidden fire in an aircraft overhead inaccessible-area is hazardous to in-flight safety and could lead to catastrophic disaster. In this case, fire detection at the earliest stage requires an improved understanding of the heat and mass transfer in overhead areas with curved fuselage sections. In this effort, an experimental campaign was conducted at
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Guo, H., Vanella, M., Lyon, R. E., McDermott, R., Crowley, S., & Scrofani, P. (2021). A Study on Experimental Tests and Numerical Simulations of Boeing 747 Overhead Inaccessible-Area Fires (Report No. DOT/FAA/TC-21/8). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57851
Guo, Haiqing, Marcos Vanella, Richard E. Lyon, Randall McDermott, Sean Crowley, and Paul Scrofani. A Study on Experimental Tests and Numerical Simulations of Boeing 747 Overhead Inaccessible-Area Fires. Report no. DOT/FAA/TC-21/8. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2021. https://rosap.ntl.bts.gov/view/dot/57851.
Guo, Haiqing, et al. A Study on Experimental Tests and Numerical Simulations of Boeing 747 Overhead Inaccessible-Area Fires. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2021, Report no. DOT/FAA/TC-21/8, ROSA P. https://rosap.ntl.bts.gov/view/dot/57851.
The Fuel Tank Flammability Assessment Method (FTFAM) is a Federal Aviation Administration-developed computer model designed as a comparative analysis tool to determine airplane fuel tank flammability as a requirement of Title 14 Code of Federal Regulations Section 25.981. The model uses Monte Carlo statistical methods to determine the average fuel
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Summer, S. M. (2021). Fuel Tank Flammability Assessment Method User's Manual - Updated for Version 11 (Report No. DOT/FAA/TC-21/3). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57849
Summer, Steven M.. Fuel Tank Flammability Assessment Method User's Manual - Updated for Version 11. Report no. DOT/FAA/TC-21/3. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2021. https://rosap.ntl.bts.gov/view/dot/57849.
Summer, Steven M. Fuel Tank Flammability Assessment Method User's Manual - Updated for Version 11. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2021, Report no. DOT/FAA/TC-21/3, ROSA P. https://rosap.ntl.bts.gov/view/dot/57849.
A physically based microscale combustion parameter for early stage fire growth, called the fire growth capacity (FGC) (J/g-K), is derived from a simple burning model. The FGC combines the ignitability and heat release of the material into a single parameter that can be measured in a microscale combustion calorimeter (MCC) using the standard ASTM D7
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Safronava, N., Lyon, R. E., & Walters, R. N. (2020). Microscale Fire Test for Component Substitutions in Aircraft Cabin Materials (Report No. DOT/FAA/TC-20/30). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57831
Safronava, Natallia, Richard E. Lyon, and Richard N. Walters. Microscale Fire Test for Component Substitutions in Aircraft Cabin Materials. Report no. DOT/FAA/TC-20/30. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2020. https://rosap.ntl.bts.gov/view/dot/57831.
Safronava, Natallia, et al. Microscale Fire Test for Component Substitutions in Aircraft Cabin Materials. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2020, Report no. DOT/FAA/TC-20/30, ROSA P. https://rosap.ntl.bts.gov/view/dot/57831.
In this study, a burning model is used to link the molecular-level processes of flaming combustion measured in thermal analysis to the fire response of a polymer at the continuum level. A flammability parameter that includes ignitability and burning rate, driven by heat release, emerging from this analysis is called the Fire Growth Capacity (FGC).
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Lyon, R. E., Safronava, N., Crowley, S., & Walters, R. N. (2020). A Physical Basis for Comparing Flammability of Aircraft Cabin Materials Using a Microscale Combustion Calorimeter (Report No. DOT/FAA/TC-20/35). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57835
Lyon, Richard E., Natallia Safronava, Sean Crowley, and Richard N. Walters. A Physical Basis for Comparing Flammability of Aircraft Cabin Materials Using a Microscale Combustion Calorimeter. Report no. DOT/FAA/TC-20/35. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2020. https://rosap.ntl.bts.gov/view/dot/57835.
Lyon, Richard E., et al. A Physical Basis for Comparing Flammability of Aircraft Cabin Materials Using a Microscale Combustion Calorimeter. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2020, Report no. DOT/FAA/TC-20/35, ROSA P. https://rosap.ntl.bts.gov/view/dot/57835.
The FAA has published two previous versions of the Aircraft Materials Fire Test Handbook: DOT/FAA/CT-89/15 and DOT/FAA/AR-00/12. The main purpose of the Handbook is to describe various fire test methods for aircraft materials in a consistent and detailed format. The Handbook provides information to enable the user to assemble and properly use certa
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Marker, T. R. (2019). Aircraft Materials Fire Test Handbook, Revision 3 (Report No. DOT/FAA/TC-17/55). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57735
Marker, Timothy R.. Aircraft Materials Fire Test Handbook, Revision 3. Report no. DOT/FAA/TC-17/55. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2019. https://rosap.ntl.bts.gov/view/dot/57735.
Marker, Timothy R. Aircraft Materials Fire Test Handbook, Revision 3. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2019, Report no. DOT/FAA/TC-17/55, ROSA P. https://rosap.ntl.bts.gov/view/dot/57735.
The prevalence of lithium batteries on aircraft is a potential safety hazard because of the risk of thermal runaway - a rapid rise in temperature and pressure, and the release of flammable gases. The goal of this study was to create a framework for potential guidelines for a standardized test method for the classification of a lithium battery's cel
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Karp, M. (2019). Thermal Runaway Initiation Methods for Lithium Batteries (Report No. DOT/FAA/TC-20/12). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57824
Karp, Matthew. Thermal Runaway Initiation Methods for Lithium Batteries. Report no. DOT/FAA/TC-20/12. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2019. https://rosap.ntl.bts.gov/view/dot/57824.
Karp, Matthew Thermal Runaway Initiation Methods for Lithium Batteries. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2019, Report no. DOT/FAA/TC-20/12, ROSA P. https://rosap.ntl.bts.gov/view/dot/57824.
Hidden fire in the aircraft cabin has been characterized as a hazardous phenomenon to in-flight safety and could lead to catastrophic disaster. Detecting hidden fire at the earliest stage is required and can be achieved only through an improved understanding of the transport of hot gases and smoke due to a possible hidden fire. This research uses t
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Guo, H., Oztekin, E. S., Crowley, S., Scrofani, P., & Lyon, R. E. (2019). Modeling of Hidden Fire in Aircraft Overhead Area (Report No. DOT/FAA/TC-18/14). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57750
Guo, Haiqing, Ezgi S. Oztekin, Sean Crowley, Paul Scrofani, and Richard E. Lyon. Modeling of Hidden Fire in Aircraft Overhead Area. Report no. DOT/FAA/TC-18/14. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2019. https://rosap.ntl.bts.gov/view/dot/57750.
Guo, Haiqing, et al. Modeling of Hidden Fire in Aircraft Overhead Area. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2019, Report no. DOT/FAA/TC-18/14, ROSA P. https://rosap.ntl.bts.gov/view/dot/57750.
The Next Generation (NexGen) (sonic) burner is a new burner designed by the FAA William J. Hughes Technical Center for the required FAA fire certification tests on power plant components. The objective of this study is to understand the performance of this burner and provide the benchmark to adapt the burner settings for future FAA fire tests. Test
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Tambe, S., Kao, Y. H., Hasselbeck, J., & Jeng, S. M. (2018). Development of Nexgen Burner Operations Setting for Fire Testing of Power Plant Components (Report No. DOT/FAA/TC-18/16). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57752
Tambe, Samir, Yi-Huan Kao, John Hasselbeck, and San-Mou Jeng. Development of Nexgen Burner Operations Setting for Fire Testing of Power Plant Components. Report no. DOT/FAA/TC-18/16. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2018. https://rosap.ntl.bts.gov/view/dot/57752.
Tambe, Samir, et al. Development of Nexgen Burner Operations Setting for Fire Testing of Power Plant Components. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2018, Report no. DOT/FAA/TC-18/16, ROSA P. https://rosap.ntl.bts.gov/view/dot/57752.
A test protocol is developed for assessing the fire hazard of a ceiling material in a combat ground vehicle. The hazards to the occupants include the thermal and toxic hazards from asphyxiant and irritant gases. An analysis is developed to determine the critical material fire properties that meet a safe level. The safe level is defined to consist o
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Quintiere, J. G., Speitel, L., Guo, H., Crowley, S., & Houston, C. Y. (2018). A Test Protocol to Define Flammability and Toxic Hazard of Ceiling Impact Protective Material (Report No. DOT/FAA/TC-17/46). United States. Army. Tank Automotive Research Development and Engineering Center (TARDEC). https://rosap.ntl.bts.gov/view/dot/57727
Quintiere, James G., Louise Speitel, Haiqing Guo, Sean Crowley, and Carleen Y. Houston. A Test Protocol to Define Flammability and Toxic Hazard of Ceiling Impact Protective Material. Report no. DOT/FAA/TC-17/46. United States. Army. Tank Automotive Research Development and Engineering Center (TARDEC), 2018. https://rosap.ntl.bts.gov/view/dot/57727.
Quintiere, James G., et al. A Test Protocol to Define Flammability and Toxic Hazard of Ceiling Impact Protective Material. United States. Army. Tank Automotive Research Development and Engineering Center (TARDEC), 2018, Report no. DOT/FAA/TC-17/46, ROSA P. https://rosap.ntl.bts.gov/view/dot/57727.
The Airport and Aircraft Safety Research and Development Group Fire Safety Team performed tests at the FAA William J. Hughes Technical Center to examine the variation in flammability exposure of fuel tanks comprised of a composite material skin and a traditional aluminum skin. The variation in topcoat color of the aluminum material was analyzed, as
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Summer, S. M. (2017). The Effects of Topcoat Color and Material Thickness on the Flammability Characteristics of Composite and Aluminum Wing Fuel Tanks (Report No. DOT/FAA/TC-17/12). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57703
Summer, Steven M.. The Effects of Topcoat Color and Material Thickness on the Flammability Characteristics of Composite and Aluminum Wing Fuel Tanks. Report no. DOT/FAA/TC-17/12. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2017. https://rosap.ntl.bts.gov/view/dot/57703.
Summer, Steven M. The Effects of Topcoat Color and Material Thickness on the Flammability Characteristics of Composite and Aluminum Wing Fuel Tanks. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2017, Report no. DOT/FAA/TC-17/12, ROSA P. https://rosap.ntl.bts.gov/view/dot/57703.
The effectiveness of aircraft depressurization (reduced pressure) on the burning behavior of stacked cargo, batteries, fuel, and materials was measured in a 381-cubic-foot (10.8-cubic-meter) pressure vessel, modified to conduct fire tests at a specific reduced pressure or programmed to vary the pressure to simulate aircraft depressurization to cont
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Burns, M., Hill, R., & Hahn, F. (2017). Cargo Fire Suppression by Depressurization (Report No. DOT/FAA/TC-17/39). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57723
Burns, Michael, Richard Hill, and Frank Hahn. Cargo Fire Suppression by Depressurization. Report no. DOT/FAA/TC-17/39. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2017. https://rosap.ntl.bts.gov/view/dot/57723.
Burns, Michael, et al. Cargo Fire Suppression by Depressurization. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2017, Report no. DOT/FAA/TC-17/39, ROSA P. https://rosap.ntl.bts.gov/view/dot/57723.
This report summarizes the research effort undertaken by the FAA to determine any differences in occupant survivability during a simulated post-crash fire when using thermoplastic paneling located in the lower seating area that meets current heat release rate requirements versus paneling that does not meet the current heat release rate requirements
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Marker, T. R. (2017). A Comparison of the Performance of OSU-Compliant versus Non-OSU-Compliant Thermoplastics Used in the Lower Area of Aircraft Seats during a Simulated Post-crash Fire Scenario (Report No. DOT/FAA/TC-16/42). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57691
Marker, Timothy R.. A Comparison of the Performance of OSU-Compliant versus Non-OSU-Compliant Thermoplastics Used in the Lower Area of Aircraft Seats during a Simulated Post-crash Fire Scenario. Report no. DOT/FAA/TC-16/42. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2017. https://rosap.ntl.bts.gov/view/dot/57691.
Marker, Timothy R. A Comparison of the Performance of OSU-Compliant versus Non-OSU-Compliant Thermoplastics Used in the Lower Area of Aircraft Seats during a Simulated Post-crash Fire Scenario. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2017, Report no. DOT/FAA/TC-16/42, ROSA P. https://rosap.ntl.bts.gov/view/dot/57691.
A series of tests was conducted to determine the effect that concentrations of hydrogen below its lower flammability limit can have on the burning of other materials. The vertical Bunsen burner test cabinet was set up to run tests with hydrogen concentrations varying between 0% and 4% by volume. Three different materials were tested: a 1/16″ thick
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Rehn, S. (2017). Flammability of Materials in a Low-Concentration Hydrogen Environment (Report No. DOT/FAA/TC-17/23). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/57710
Rehn, Steven. Flammability of Materials in a Low-Concentration Hydrogen Environment. Report no. DOT/FAA/TC-17/23. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2017. https://rosap.ntl.bts.gov/view/dot/57710.
Rehn, Steven Flammability of Materials in a Low-Concentration Hydrogen Environment. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2017, Report no. DOT/FAA/TC-17/23, ROSA P. https://rosap.ntl.bts.gov/view/dot/57710.
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