Andere Kunden interessierten sich auch für
![Effects of Prior Aging At 288°C in Argon Environment on Creep Response of Carbon Fiber Reinforced PMR-15 Composite with ±45° Fiber Orientation at 288°]( "Effects of Prior Aging At 288°C in Argon Environment on Creep Response of Carbon Fiber Reinforced PMR-15 Composite with ±45° Fiber Orientation at 288°")
Effects of Prior Aging At 288°C in Argon Environment on Creep Response of Carbon Fiber Reinforced PMR-15 Composite with ±45° Fiber Orientation at 288°59,99 €![Fabrication and Evaluation of Graphite Fiber-Reinforced Polyimide Composite Tube Forms Using Modified Resin Transfer Molding]( "Fabrication and Evaluation of Graphite Fiber-Reinforced Polyimide Composite Tube Forms Using Modified Resin Transfer Molding")
Fabrication and Evaluation of Graphite Fiber-Reinforced Polyimide Composite Tube Forms Using Modified Resin Transfer Molding60,99 €![Characterization of Graphite Composite Material Particulates from United States Air Force Aircraft Maintenance Operations]( "Characterization of Graphite Composite Material Particulates from United States Air Force Aircraft Maintenance Operations")
Characterization of Graphite Composite Material Particulates from United States Air Force Aircraft Maintenance Operations59,99 €![Examination of Air Force Crash Damage or Disabled Aircraft Recovery Program Resourcing]( "Examination of Air Force Crash Damage or Disabled Aircraft Recovery Program Resourcing")
Examination of Air Force Crash Damage or Disabled Aircraft Recovery Program Resourcing60,99 €![Mechanical Properties Characterization and Business Case Analysis of the Fiber Metal Laminate GLARE-3 for Use as Secondary Aircraft Structure]( "Mechanical Properties Characterization and Business Case Analysis of the Fiber Metal Laminate GLARE-3 for Use as Secondary Aircraft Structure")
Mechanical Properties Characterization and Business Case Analysis of the Fiber Metal Laminate GLARE-3 for Use as Secondary Aircraft Structure59,99 €![Characterization and Control of Carbon Dioxide Seed Particles in Particle Image Velocimetry]( "Characterization and Control of Carbon Dioxide Seed Particles in Particle Image Velocimetry")
Characterization and Control of Carbon Dioxide Seed Particles in Particle Image Velocimetry59,99 €![Classification Characteristics of Carbon Nanotube Polymer Composite Chemical Vapor Detectors]( "Classification Characteristics of Carbon Nanotube Polymer Composite Chemical Vapor Detectors")
Classification Characteristics of Carbon Nanotube Polymer Composite Chemical Vapor Detectors60,99 €
Within the United States Air Force (USAF) Advanced Composite Material (ACM) is gaining an increasing use in military aircraft. With the number of aircraft that have increasingly large amounts of ACM materials, the probability of an incident with one of these aircraft also increases. When such an incident occurs the aircraft needs to be disassembled, removed, and later inspected as part of the accident investigation process. This disassembly process is termed "Crash Recovery Operations." Carbon fibers have been shown to be hazardous to human health and a pilot study raised the suspicion that nanosized aerosol may be generated during the cutting of carbon fiber panels. Due to this, a bench top study was conducted to evaluate the effectiveness of several fiber controls. Additionally, an evaluation of a number of direct reading instruments and traditional gravimetric sampling techniques were evaluated to determine a sampling protocol for evaluation composite fibers.