The usage and integrated vehicle health management of the NASA C-17. Propulsion health management flight objectives for the aircraft include mapping of the High Pressure Compressor in order to calibrate a Pratt and Whitney engine model and the fusion of data collected from existing sensors and signals to develop models, analysis methods and information fusion algorithms. An additional health manage flight objective is to demonstrate that the Commercial Modular Aero-Propulsion Systems Simulation engine model can successfully execute in real time onboard the C-17 T-1 aircraft using engine and aircraft flight data as inputs. Future work will address aircraft durability and aging, airframe health management, and propulsion health management res...
Turbine engine failures are the leading cause of class-A mechanical failures (loss of aircraft). The...
Overview of the Vehicle Integrated Propulsion Research Tests in the Vehicle Systems Safety Technolog...
The work reported herein represents a continuation of work begun at MSFC during the 1991 NASA/ASEE S...
Develop Advanced Sensor Technology and rotordynamic structural diagnostics to address existing Aviat...
The following subject areas are covered: hierarchy of civil space technology program; evolution of t...
NASA is reviewing various propulsion technologies for exploring space. The requirements are examined...
The Intelligent Control and Autonomy Branch (ICA) at NASA (National Aeronautics and Space Administra...
227921360Technical memorandumNTIS Invoice: 21909;NTIS Order #:ADA376621PDFProceedingsNASA/TM-2000-21...
The ERA project was created in 2009 as part of NASAs Aeronautics Research Mission Directorates (ARMD...
Structural Health Management (SHM) will be of critical importance to provide the safety, reliability...
Structural Health Management (SHM) will be of critical importance to provide the safety, reliability...
This report presents the results of the NASA contract Propulsion System Health Management for Enhanc...
Since its founding, NASA has been dedicated to the advancement of aeronautics and space science. The...
Various engine related performance and health monitoring techniques developed in support of flight r...
The Commercial Aero-Propulsion Control Working Group (CAPCWG), consisting of propulsion control tech...
Turbine engine failures are the leading cause of class-A mechanical failures (loss of aircraft). The...
Overview of the Vehicle Integrated Propulsion Research Tests in the Vehicle Systems Safety Technolog...
The work reported herein represents a continuation of work begun at MSFC during the 1991 NASA/ASEE S...
Develop Advanced Sensor Technology and rotordynamic structural diagnostics to address existing Aviat...
The following subject areas are covered: hierarchy of civil space technology program; evolution of t...
NASA is reviewing various propulsion technologies for exploring space. The requirements are examined...
The Intelligent Control and Autonomy Branch (ICA) at NASA (National Aeronautics and Space Administra...
227921360Technical memorandumNTIS Invoice: 21909;NTIS Order #:ADA376621PDFProceedingsNASA/TM-2000-21...
The ERA project was created in 2009 as part of NASAs Aeronautics Research Mission Directorates (ARMD...
Structural Health Management (SHM) will be of critical importance to provide the safety, reliability...
Structural Health Management (SHM) will be of critical importance to provide the safety, reliability...
This report presents the results of the NASA contract Propulsion System Health Management for Enhanc...
Since its founding, NASA has been dedicated to the advancement of aeronautics and space science. The...
Various engine related performance and health monitoring techniques developed in support of flight r...
The Commercial Aero-Propulsion Control Working Group (CAPCWG), consisting of propulsion control tech...
Turbine engine failures are the leading cause of class-A mechanical failures (loss of aircraft). The...
Overview of the Vehicle Integrated Propulsion Research Tests in the Vehicle Systems Safety Technolog...
The work reported herein represents a continuation of work begun at MSFC during the 1991 NASA/ASEE S...