Brief: Discover the AITM 2.0006 Heat Release Rate OSU Tester, designed for aviation materials compliance with FAR Part 25 Appendix F Part IV. This FAA-approved tester measures heat release rates with precision, featuring a stainless steel combustion chamber and advanced heat flux control. Ideal for Airbus AITM 2.0006 and Boeing BSS 7322 standards.
Related Product Features:
Stainless steel combustion test chamber with high-temperature glass observation window.
Four Glowbars heating rods providing 35KW/M2 heat radiation flux.
Dual PID temperature controllers for precise heating control.
Fully automatic pneumatic sample propulsion and shielding door device.
Upper and lower burners with adjustable gas flow via rotor flowmeter.
Water-cooled heat flow meter for accurate heat radiation flux measurement.
Data acquisition system with heat release standard test software.
Complies with AITM 2.0006, BSS 7322, and FAR PART 25 Appendix F Part IV standards.
Perguntas frequentes:
What standards does the OSU Heat Release Rate Tester comply with?
The tester complies with FAR Part 25 Appendix F Part IV, Airbus AITM 2.0006, and Boeing BSS 7322 standards.
What is the heat flux density provided by the radiant heat source?
The radiant heat source provides a heat flux density of 35±0.5kW/m2.
What materials are used in the construction of the test chamber?
The test chamber is constructed of corrosion-resistant stainless steel, including the housing, reflector, and mask.