Search Results
AIRCRAFT DATA INTERFACE FUNCTION (ADIF)
MEDIA INDEPENDENT SECURE OFFBOARD NETWORK
Spotlight on Design Insight: Fuel Efficiency: Fuel Economy Testing
Fiber Optic Strain Sensor Standardization - International and European Activities
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
Laser-Assisted Filler-Based Joining for Battery Assembly in Aviation
Raw Measurements from Global Navigation Satellite System (GNSS) Receivers
Security and Resilience Recommendations for Positioning, Navigation, and Timing (PNT) Users
Inertial Measurement Unit (IMU) Interface Requirements for Military and Aerospace Vehicle Applications
Simulated Inertial Measurement Unit (IMU) Interface Requirements for Military and Aerospace Vehicle Applications
Test Plan for the SAE2020 Inertial Measurement Unit (IMU) Interface
Global eLoran User Equipment Interface Standard
Global eLoran User Equipment Interface Standard for Timing
Guidelines for Resilient GNSS Receivers
Standard for Interfacing Resilient GNSS Receivers
Receiver Standard for the Transmitted eLoran Signal
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
This Aerospace Information Report (AIR) is a historical technical record describing procedures, required continuous sampling conditions, and instrumentation for the measurement of non-volatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to calculate sampling loss performance. This AIR is not intended for in-flight testing, nor does it apply to engine operating in the afterburning mode.
This Aerospace Information Report is a historical technical record of the initial document detailing the measurement of non-volatile particle emissions at the exit plane of aircraft gas turbine engines. This methodology was adopted by ICAO into Annex 16 Vol II and updated into Aerospace Recommended Practice ARP6320.
Future updates of this document may include explanations of the reasoning and assumptions used to develop this measurement methodology.