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Supplier: ASTM International
Description: in the quick disconnects (QDs) in the environmental control and life support system (ECLSS) on the International Space Station (ISS). Testing included standard supersonic and subsonic particle impact tests on 15 - 5 PH stainless steel, as well as tests performed on a QD simulator. This paper summarizes
Standards and Technical Documents - Environmental tests for aircraft equipment -- Part 3.4 : Acoustic vibration -- ISO 2671:1982
Description: Specifies laboratory conditions for testing the ability of equipment for subsonic and supersonic civil aircraft to withstand vibration. Two types of tests are specified: tests for the functioning of the equipment and tests for its acoustic endurance. The necessity of such tests, the use of the wide
Standards and Technical Documents - Overview of the ICE Project: Integration of Computational Fluid Dynamics and Experiments - 47th IIS 2001
Description: of a supersonic inlet, real-time data visualization and display, low-speed compressor testing, and a parallel-processing simulation code interface for multistage turbomachinergy. A detailed data model for the compressor application is included in the appendix.
Standards and Technical Documents - Environmental testing - Part 2-10: Tests - Test J and guidance: Mould growth -- IEC 60068-2-10:2005
Description: - Spores suspension in mineral salt solution additionally introduced - Pre-conditioning of the specimens by damp heat storage prescribed - Supersonic aerosolization of the spores suspension as the preferred inoculation method introduced - Duration of incubation reduced from 84 days to 56 days - Extent
Standards and Technical Documents - Graphical method for the analysis of measured performance data using drag determination: aircraft with turbo-jet and turbo-fan engines. -- 70021Supplier: IHS ESDU
Description: RJ2/1, but it enables greater use to be made of the flight time and is less demanding on pilot technique. It is applicable in the subsonic and supersonic flight regimes. The theory is outlined in ESDU 70020 which also indicates the limitations of the non-dimensional approach used in ESDU 70021
Supplier: Boeing Company (The)
Description: , 2013, at Tyndall Air Force Base, Fla. The QF-16 mission profile included auto takeoff, a series of simulated maneuvers, supersonic flight and an auto land all without a pilot in the cockpit. Testing on the six aircraft continues at Holloman Air Force Base, N.M. Technical Specifications Primary
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Military/Commercial Specifications and Standards
RTCA/DO-160 Testing. E-Labs can test to RTCA/DO-160 which covers standard procedures and environmental test criteria for testing airborne electronic equipment (avionics) for the entire spectrum of aircraft, from light general aviation aircraft and helicopters through to the "jumbo jet" and "supersonic transport" classes of aircraft. RTCA/DO-160 Dynamic and Vibration Testing Services: MIL-STD-167-1. Section 4 Temperature and Altitude. Section 5 Temperature Variation. Section 6 Humidity. Section... (read more)
Browse Certification Services Datasheets for E-Labs, Inc.
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F/A-18 Fighter Aircraft Wing Fatigue Testing
Before any of the U.S. Navy's F/A-18 twin-engine supersonic fighter jets can be put into operation, the wings of the aircraft must undergo fatigue testing in a controlled environment to ensure that they are capable of withstanding the forces that will be encountered during real-world flight
The Joint Strike Fighter: A plane for all reasons
The X-35 JSF will be a supersonic bomber, a stealthy fighter, and a short-take-off, vertically landing warplane flown by U.S. Navy, Air Force, and Marine pilots, as well as the British armed forces. U.S. Marines will be able to land and take-off vertically with the JSF The Pratt & Whitney engine
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Ultrasound diagnosis in obstetrics and gynecology
A pregnancy care without scan is equally unthinkable like a gynaecological aligned practice without sonography apparatus.
Gynecology and obstetrics
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Ultrasound primer Internal medicine
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Reactor safety for power nuclear power stations
883 10.4.2 ultrasonic testing of pressure preceding ends enclosure.
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Billing hedgehog 2015
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