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.
This report documents the findings of a series of tests conducted to determine the flammability characteristics of primary lithium batteries and the dangers associated with shipping them in bulk form on commercial transport category aircraft.
Webster, H. (2004). Flammability Assessment of Bulk-Packed, Nonrechargeable Lithium Primary Batteries in Transport Category Aircraft Final Report (Report No. DOT/FAA/AR-04/26). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/71623
Webster, Harry. Flammability Assessment of Bulk-Packed, Nonrechargeable Lithium Primary Batteries in Transport Category Aircraft Final Report. Report no. DOT/FAA/AR-04/26. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2004. https://rosap.ntl.bts.gov/view/dot/71623.
Webster, Harry Flammability Assessment of Bulk-Packed, Nonrechargeable Lithium Primary Batteries in Transport Category Aircraft Final Report. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2004, Report no. DOT/FAA/AR-04/26, ROSA P. https://rosap.ntl.bts.gov/view/dot/71623.
This technical note presents the data from simulated aerosol can explosion tests while using bromotrifluoropropene (BTP) and pentafluoroethane (HFC-125) as fire suppression agents for aircraft cargo compartments. These explosion tests were conducted at below inert volumetric concentrations to determine the agent's explosion attenuation performance.
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Reinhardt, J. W. (2004). Behavior of Bromotrifluoropropene and Pentafluoroethane When Subjected to a Simulated Aerosol Can Explosion (Report No. DOT/FAA/AR-TN04/4). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89861
Reinhardt, John W.. Behavior of Bromotrifluoropropene and Pentafluoroethane When Subjected to a Simulated Aerosol Can Explosion. Report no. DOT/FAA/AR-TN04/4. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2004. https://rosap.ntl.bts.gov/view/dot/89861.
Reinhardt, John W. Behavior of Bromotrifluoropropene and Pentafluoroethane When Subjected to a Simulated Aerosol Can Explosion. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2004, Report no. DOT/FAA/AR-TN04/4, ROSA P. https://rosap.ntl.bts.gov/view/dot/89861.
This report discusses experiments to determine the reduction in oxygen concentration required to prevent a fuel tank explosion. A simulated aircraft fuel tank containing JP-8 fuel of an amount equivalent to a mass loading of approximately 4.5 kg/m3 was used to determine the limiting oxygen concentration (LOC) at pressures corresponding to altitudes
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Summer, S. M. (2003). Limiting Oxygen Concentration Required to Inert Jet Fuel Vapors Existing at Reduced Fuel Tank Pressures (Report No. DOT/FAA/AR-TN02/79). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89835
Summer, Steven M.. Limiting Oxygen Concentration Required to Inert Jet Fuel Vapors Existing at Reduced Fuel Tank Pressures. Report no. DOT/FAA/AR-TN02/79. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2003. https://rosap.ntl.bts.gov/view/dot/89835.
Summer, Steven M. Limiting Oxygen Concentration Required to Inert Jet Fuel Vapors Existing at Reduced Fuel Tank Pressures. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2003, Report no. DOT/FAA/AR-TN02/79, ROSA P. https://rosap.ntl.bts.gov/view/dot/89835.
The Federal Aviation Administration (FAA) is planning a series of ground and flight tests with Airbus to prove the concept of a simplified fuel tank inerting system, which has been developed by the FAA. The FAA has also developed an onboard oxygen analysis system to measure the oxygen concentration in the aircraft fuel tank during the testing. To h
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Burns, M., & Cavage, W. M. (2003). A Description and Analysis of the FAA Onboard Oxygen Analysis System (Report No. DOT/FAA/AR-TN03/52). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89854
Burns, Michael and William M. Cavage. A Description and Analysis of the FAA Onboard Oxygen Analysis System. Report no. DOT/FAA/AR-TN03/52. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2003. https://rosap.ntl.bts.gov/view/dot/89854.
Burns, Michael, and William M. Cavage A Description and Analysis of the FAA Onboard Oxygen Analysis System. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2003, Report no. DOT/FAA/AR-TN03/52, ROSA P. https://rosap.ntl.bts.gov/view/dot/89854.
This report documents a series of tests to determine the amount of positive pressure differential between the flight deck and surrounding areas necessary to prevent smoke from penetrating into the flight deck. The testing also explored methods to demonstrate the effectiveness of those ventilation conditions. The tests were conducted on the ground i
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Blake, D. (2003). Ground Tests of Aircraft Flight Deck Smoke Penetration Resistance (Report No. DOT/FAA/AR-TN03/36). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89853
Blake, David. Ground Tests of Aircraft Flight Deck Smoke Penetration Resistance. Report no. DOT/FAA/AR-TN03/36. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2003. https://rosap.ntl.bts.gov/view/dot/89853.
Blake, David Ground Tests of Aircraft Flight Deck Smoke Penetration Resistance. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2003, Report no. DOT/FAA/AR-TN03/36, ROSA P. https://rosap.ntl.bts.gov/view/dot/89853.
This technical note presents the updated version of the minimum performance standards (MPS) that a Halon 1301 replacement or alternate system for aircraft cargo compartment must meet as part of the aircraft certification procedures. This standard considers gaseous and nongaseous fire suppression systems for full-scale fire testing. The Federal Avia
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Reinhardt, J. W. (2003). Minimum Performance Standard for Aircraft Cargo Compartment Halon Replacement Fire Suppression Systems (Report No. DOT/FAA/AR-TN03/6). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89838
Reinhardt, John W.. Minimum Performance Standard for Aircraft Cargo Compartment Halon Replacement Fire Suppression Systems. Report no. DOT/FAA/AR-TN03/6. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2003. https://rosap.ntl.bts.gov/view/dot/89838.
Reinhardt, John W. Minimum Performance Standard for Aircraft Cargo Compartment Halon Replacement Fire Suppression Systems. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2003, Report no. DOT/FAA/AR-TN03/6, ROSA P. https://rosap.ntl.bts.gov/view/dot/89838.
The purpose of this testing was to determine the temperatures that would cause self-activation of sodium chlorate oxygen generators. The data will be used to establish the degree of thermal protection that would be required to prevent the activation of chemical oxygen generators should they be exposed to heat from cargo compartment fire involving o
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Blake, D. (2003). The Response of Aircraft Oxygen Generators Exposed to Elevated Temperatures (Report No. DOT/FAA/AR-TN03/35). United States. Department of Transportation. Federal Aviation Administration. https://rosap.ntl.bts.gov/view/dot/16408
Blake, David. The Response of Aircraft Oxygen Generators Exposed to Elevated Temperatures. Report no. DOT/FAA/AR-TN03/35. United States. Department of Transportation. Federal Aviation Administration, 2003. https://rosap.ntl.bts.gov/view/dot/16408.
Blake, David The Response of Aircraft Oxygen Generators Exposed to Elevated Temperatures. United States. Department of Transportation. Federal Aviation Administration, 2003, Report no. DOT/FAA/AR-TN03/35, ROSA P. https://rosap.ntl.bts.gov/view/dot/16408.
The Ohio State University (OSU) Rate of Heat Release Apparatus specified in FAR Part 25.853(a-1) defines both apparatus test conditions and pass/fail criteria for large surface area aircraft interior materials, such as sidewall panels, bulkheads, and stowage bins. The cone calorimeter (ASTM E-1354 Standard Test Method for Heat and Visible Smoke Rel
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Filipczak, R. Z., & Lyon, R. E. (2002). The Correlation of Heat Release Calorimetry Measurements (Report No. DOT/FAA/AR-TN02/104). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89836
Filipczak, Robert Z. and Richard E. Lyon. The Correlation of Heat Release Calorimetry Measurements. Report no. DOT/FAA/AR-TN02/104. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2002. https://rosap.ntl.bts.gov/view/dot/89836.
Filipczak, Robert Z., and Richard E. Lyon The Correlation of Heat Release Calorimetry Measurements. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2002, Report no. DOT/FAA/AR-TN02/104, ROSA P. https://rosap.ntl.bts.gov/view/dot/89836.
The purpose of this technical note is to document the results of fire tests conducted to examine the characteristics of fire that may occur in the cavity of an aircraft seat armrest and the fire-containment capacity of the cavity. In all the tests the armrest materials did not ignite, and the fire was contained within the armrest cavity.
Johnson, R. M. (2002). Burning Behavior Within a Seat Armrest Cavity (Report No. DOT/FAA/AR-TN02/105). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/16409
Johnson, Richard M.. Burning Behavior Within a Seat Armrest Cavity. Report no. DOT/FAA/AR-TN02/105. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2002. https://rosap.ntl.bts.gov/view/dot/16409.
Johnson, Richard M. Burning Behavior Within a Seat Armrest Cavity. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2002, Report no. DOT/FAA/AR-TN02/105, ROSA P. https://rosap.ntl.bts.gov/view/dot/16409.
One or more Halon 1211 hand-held fire extinguishers are specified in Federal Aviation Regulation (FAR) Part 25.851 as a requirement on transport category aircraft with 31 or more seats. Halon 1211 has been linked to the destruction of the ozone layer and production of new Halon 1211 has been halted per the Montreal Protocol in 1993. The phase out o
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Webster, H. (2002). Development of a Minimum Performance Standard for Hand-Held Fire Extinguishers as a Replacement for Halon 1211 on Civilian Transport Category Aircraft (Report No. DOT/FAA/AR-01/37). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/16410
Webster, Harry. Development of a Minimum Performance Standard for Hand-Held Fire Extinguishers as a Replacement for Halon 1211 on Civilian Transport Category Aircraft. Report no. DOT/FAA/AR-01/37. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2002. https://rosap.ntl.bts.gov/view/dot/16410.
Webster, Harry Development of a Minimum Performance Standard for Hand-Held Fire Extinguishers as a Replacement for Halon 1211 on Civilian Transport Category Aircraft. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2002, Report no. DOT/FAA/AR-01/37, ROSA P. https://rosap.ntl.bts.gov/view/dot/16410.
Molecular design of semi-inorganic rubbers has yielded flexible polysilphenylene-siloxane and polyphosphazene elastomers having the fire resistance of rigid, high-temperature engineering plastics (e.g., polyaramids, polyetherketones, and polyarylsulfones) based on the results of microscale combustibility data. In flaming combustion, a commercially
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Lyon, R. E. (2002). Fire-Resistant Elastomers (Report No. DOT/FAA/AR-TN01/104). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89805
Lyon, Richard E.. Fire-Resistant Elastomers. Report no. DOT/FAA/AR-TN01/104. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2002. https://rosap.ntl.bts.gov/view/dot/89805.
Lyon, Richard E. Fire-Resistant Elastomers. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2002, Report no. DOT/FAA/AR-TN01/104, ROSA P. https://rosap.ntl.bts.gov/view/dot/89805.
A method for measuring the heat release rate of milligram-sized samples is described in this report. Pyrolysis-combustion flow calorimetry (PCFC) separately reproduces the solid-state and gas phase processes of flaming combustion in a non-flaming test by rapid controlled pyrolysis of the sample in an inert gas stream followed by high-temperature ox
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Lyon, R. E., & Walters, R. (2002). A Microscale Combustion Calorimeter (Report No. DOT/FAA/AR-01/117). United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research. https://rosap.ntl.bts.gov/view/dot/92726
Lyon, Richard E. and Richard Walters. A Microscale Combustion Calorimeter. Report no. DOT/FAA/AR-01/117. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 2002. https://rosap.ntl.bts.gov/view/dot/92726.
Lyon, Richard E., and Richard Walters A Microscale Combustion Calorimeter. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 2002, Report no. DOT/FAA/AR-01/117, ROSA P. https://rosap.ntl.bts.gov/view/dot/92726.
This report documents the full-scale evaluation tests of a water mist system, with and without nitrogen that would be available from an onboard inert gas generation system (OBIGGS) against a series of standardized aircraft cargo fires.
Reinhardt, J. W. (2002). Evaluation of Water Mist With and Without Nitrogen as an Aircraft Cargo Compartment Fire Suppression System (Report No. DOT/FAA/AR-01/121). United States. Department of Transportation. Federal Aviation Administration. https://rosap.ntl.bts.gov/view/dot/41765
Reinhardt, J. W.. Evaluation of Water Mist With and Without Nitrogen as an Aircraft Cargo Compartment Fire Suppression System. Report no. DOT/FAA/AR-01/121. United States. Department of Transportation. Federal Aviation Administration, 2002. https://rosap.ntl.bts.gov/view/dot/41765.
Reinhardt, J. W. Evaluation of Water Mist With and Without Nitrogen as an Aircraft Cargo Compartment Fire Suppression System. United States. Department of Transportation. Federal Aviation Administration, 2002, Report no. DOT/FAA/AR-01/121, ROSA P. https://rosap.ntl.bts.gov/view/dot/41765.
A task group assembled under the auspices of the International Aircraft Materials Fire Test Working Group examined issues involving fire test approval of previously qualified interior material systems following renovation or alteration. A major problem associated with the alteration of interior system components is the difficulty in conducting cert
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Marker, T. (2001). Heat Release and Flammability Testing of Surrogate Panels (Report No. DOT/FAA/AR-TN01/112). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89802
Marker, Timothy. Heat Release and Flammability Testing of Surrogate Panels. Report no. DOT/FAA/AR-TN01/112. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001. https://rosap.ntl.bts.gov/view/dot/89802.
Marker, Timothy Heat Release and Flammability Testing of Surrogate Panels. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001, Report no. DOT/FAA/AR-TN01/112, ROSA P. https://rosap.ntl.bts.gov/view/dot/89802.
A new fire extinguisher concept, the adiabatic expansion nozzle, extends the usefulness of fire extinguishing compounds by lowering the temperature and discharge pressure of the agent. This allows total flood type halon replacements to be used in handheld applications and, in the instance of carbon dioxide, produces a low-pressure dry ice snow.
Filipczak, R. Z. (2001). Development and Performance of an Adiabatic Expansion Nozzle for Improved Fire Extinguishers (Report No. DOT/FAA/AR-TN01/60). United States. Department of Transportation. Federal Aviation Administration. https://rosap.ntl.bts.gov/view/dot/40826
Filipczak, Robert Z.. Development and Performance of an Adiabatic Expansion Nozzle for Improved Fire Extinguishers. Report no. DOT/FAA/AR-TN01/60. United States. Department of Transportation. Federal Aviation Administration, 2001. https://rosap.ntl.bts.gov/view/dot/40826.
Filipczak, Robert Z. Development and Performance of an Adiabatic Expansion Nozzle for Improved Fire Extinguishers. United States. Department of Transportation. Federal Aviation Administration, 2001, Report no. DOT/FAA/AR-TN01/60, ROSA P. https://rosap.ntl.bts.gov/view/dot/40826.
Child restraint seat used in aircraft are based on automotive designs that are required to pass a horizontal burn rate test method. The flammability of child seat materials was gauged against the Federal Aviation Administration (FAA) vertical Bunsen burner tests method. Basically, the vertical test prescribed in Federal Aviation Regulation (FAR) 25
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Johnson, R., & Wuethrich, L. (2001). Flammability of Automotive Child Restraint Seats for Use in Aircraft (Report No. DOT/FAA/AR-TN01/42). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89800
Johnson, R. and Lindsey Wuethrich. Flammability of Automotive Child Restraint Seats for Use in Aircraft. Report no. DOT/FAA/AR-TN01/42. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001. https://rosap.ntl.bts.gov/view/dot/89800.
Johnson, R., and Lindsey Wuethrich Flammability of Automotive Child Restraint Seats for Use in Aircraft. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001, Report no. DOT/FAA/AR-TN01/42, ROSA P. https://rosap.ntl.bts.gov/view/dot/89800.
The Federal Aviation Administration (FAA) has developed a unique extractive Fourier Transform Infrared (FTIR) system to analyze rapidly changing moist fire gas concentrations as a function of time. The system was designed to eliminate numerous errors generated by state-of-the-art FTIR systems for fire gas analysis. In addition, the path length, cel
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Speitel, L. (2001). Fourier Transform Infrared Analysis of Combustion Gases (Report No. DOT/FAA/AR-01/88). United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research. https://rosap.ntl.bts.gov/view/dot/92720
Speitel, Louise. Fourier Transform Infrared Analysis of Combustion Gases. Report no. DOT/FAA/AR-01/88. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 2001. https://rosap.ntl.bts.gov/view/dot/92720.
Speitel, Louise Fourier Transform Infrared Analysis of Combustion Gases. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 2001, Report no. DOT/FAA/AR-01/88, ROSA P. https://rosap.ntl.bts.gov/view/dot/92720.
Polycyanurate networks were prepared by thermal polymerization of cyanate ester monomers containing two or more cyanate ester (-O-C≡N) functional groups. The thermal decomposition chemistry of nine different polycyanurates was studied by thermogravimetry and infrared analysis of solid films and analysis of the gases evolved during pyrolysis using i
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Ramirez, M. L., Walters, R., Savitski, E. P., & Lyon, R. E. (2001). Thermal Decomposition of Cyanate Ester Resins (Report No. DOT/FAA/AR-01/32). United States. Federal Aviation Administration. Office of Aviation Research. https://rosap.ntl.bts.gov/view/dot/15466
Ramirez, M. L., R. Walters, E. P. Savitski, and R. E. Lyon. Thermal Decomposition of Cyanate Ester Resins. Report no. DOT/FAA/AR-01/32. United States. Federal Aviation Administration. Office of Aviation Research, 2001. https://rosap.ntl.bts.gov/view/dot/15466.
Ramirez, M. L., et al. Thermal Decomposition of Cyanate Ester Resins. United States. Federal Aviation Administration. Office of Aviation Research, 2001, Report no. DOT/FAA/AR-01/32, ROSA P. https://rosap.ntl.bts.gov/view/dot/15466.
Specific heat release rate is the molecular-level fire response of a burning polymer. The Federal Aviation Administration (FAA) obtains the specific heat release rate of milligram samples by analyzing the oxygen consumed by complete combustion of the pyrolysis gases during a linear heating program. Dividing the specific heat release rate (W/g) by t
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Walters, R., & Lyon, R. E. (2001). Calculating Polymer Flammability from Molar Group Contributions (Report No. DOT/FAA/AR-01/31). United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research. https://rosap.ntl.bts.gov/view/dot/92724
Walters, Richard and Richard E. Lyon. Calculating Polymer Flammability from Molar Group Contributions. Report no. DOT/FAA/AR-01/31. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 2001. https://rosap.ntl.bts.gov/view/dot/92724.
Walters, Richard, and Richard E. Lyon Calculating Polymer Flammability from Molar Group Contributions. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 2001, Report no. DOT/FAA/AR-01/31, ROSA P. https://rosap.ntl.bts.gov/view/dot/92724.
Experimental results for the gross heat of combustion of over 140 commercial and developmental polymers and small molecules of known chemical structures were used to derive additive molar group contributions. Predicted gross heats of combustion were within 2.5 percent of the values measured by oxygen bomb calorimetry.
Walters, R. N. (2001). Molar Group Contributions to the Heat of Combustion (Report No. DOT/FAA/AR-TN01/75). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89803
Walters, Richard N.. Molar Group Contributions to the Heat of Combustion. Report no. DOT/FAA/AR-TN01/75. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001. https://rosap.ntl.bts.gov/view/dot/89803.
Walters, Richard N. Molar Group Contributions to the Heat of Combustion. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001, Report no. DOT/FAA/AR-TN01/75, ROSA P. https://rosap.ntl.bts.gov/view/dot/89803.
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