Products & ServicesSee also: Categories | Featured Products | Technical Articles | More Information
Standards and Technical Documents - API STD 6A -- SPECIFICATION FOR WELLHEAD EQUIPMENT (PRODUCTION VALVES, FLANGES, BLOWOUT PREVENTERS, AND WELLHEAD FITTINGS)Supplier: American Petroleum Institute (API)
Description: . 13 Segmented Flanges Sect. 14 Underwater Wellhead Equipment Many of the foregoing items of equipment have specific complementary internal dimensions to pennant (1) drilling-through, (2) running and landing a smaller string of pipe as diagrammatically shown in Fig. 1.1, (3) running tools, instruments
Supplier: Airbus Group
Description: , dual-duplex autopilot provides outstanding precision and stability and enables flight in search and rescue patterns as well as automatic approaches in instrument flight rules (IFR) procedures. Unrivalled redundancy is provided in key onboard systems to maintain full functionality, including
Supplier: Embraer S.A.
Description: configuration data redundancy to display both PFD and EICAS formats ENGINE INDICATON & CREW ALERTING SYSTEM (EICAS) is used to monitor: system indications engine & APU information cabin pressurization information fuel information flap/speed brake settings landing gear trim positions Airlines can
Supplier: Cessna Aircraft Company
Description: master caution/master warning lights LH and RH engine fire control switches Flight director/autopilot controller Electronic standby instrument system LH and RH display control units Installed on instrument panel (left to right): LH primary flight display (PFD) Multifunction display (MFD) RH
Supplier: Airbus Group
Description: ATA 31 : Instruments ATA 32 : Landing Gear ATA 34 : Navigation ATA 35 : Oxygen ATA 38 : Water / Waste ATA 42 : Integrated Modular Avionics ATA 44 : Cabin systems ATA 46 : Information System ATA 49 : Auxiliary power unit ATA 52 : Doors ATAs from 73 to 80 : Engine
- Type / Form Factor: Test Platform / System
- Components / Products Tested: Avionics / Military Electronics
Supplier: Diamond Aircraft
Description: system Fire extinguisher 3 point inertia reel safety harness (all seats) Instrument lighting Overhead cabin lights Standard interior (fabric seats with grey leather trim) Hydraulic retractable landing gear Heated pitot / static tube Alternate static port Enlarged panoramic canopy Electric
Supplier: Beechcraft Corporation
Description: of targets, and turbulence detection to help avoid severe weather. This system is designed to interface with the Primary Flight Display (PFD), Multi-Function Flight Display (MFD) and the Electronic Flight Instrument System (EFIS). Threat Awareness The Traffic Collision Avoidance System (TCAS) provides
Supplier: KLA-Tencor Corporation
Description: charge control, e-Control™, and wide landing energy) provide sensitivity on charge-sensitive layers and on advanced materials, such as low-k dielectrics and SOI Inline automatic defect classification provides nuisance filtering, reduces the defect population requiring off-line review, and enables
- Form Factor: Wafer Probing System
- Mounting / Loading: Floor Mounted / Stand-alone
- Applications: Semiconductor Wafers, Etching - Plasma / Wet, Polishing / CMP
- Measurement Capability: Defects / ADC
Find Suppliers by Category Top
Featured Products Top
maxon precision motors, inc.
Successful Landing on Comet Chury.
successfully guided its lander Philae to touch down on the four-kilometer Comet 67P/Churyumov-Gerasimenko, a.k.a. Chury. The Philae lander has a mass of 100 kg and features ten instruments. maxon motor is proud to be part of this mission. The Swiss-based drive specialist provided two DC motors, with a diameter of 13 mm each. These motors will be used to lower the APXS instrument to the ground. The APXS is an alpha x-ray spectrometer, developed by the Johannes Gutenberg University Mainz to be used... (read more)
Browse Datasheets for maxon precision motors, inc.
Rosetta Space Probe Lands on Comet after 10 years
A First in Space History – Rosetta Space Probe Lands on Comet after Ten Years of Travel. At the end of May 2014, the Rosetta space probe moved into an orbit around the comet 67P/Churyumov-Gerasimenko in order to, map its surface and prepare for the landing of Philae. This ballistic lander, weighing 100 kg, landed successfully on the comet on November, 12th 2014. The probe is powered by FAULHABER DC motors to ensure a secure landing. After an adventurous journey of over 10 years... (read more)
Browse DC Motors Datasheets for MICROMO
Omnetics Connector Corporation
Ruggedized Strip Connectors
and more portable. Ruggedness has become critical in many of the new uses for portable electronics. Unmanned aerial vehicles require low weight and small size but also demand rugged performance, especially during landing. Land based robotic circuits have high shock and continuous vibration requirements and contain field replaceable modules that need to be switched quickly. Missile systems use strip connectors that can handle the 1 amp of current in a small and low profile... (read more)
Browse Military (MIL-SPEC) Connectors Datasheets for Omnetics Connector Corporation
Conduct Research Top
ILS Monitor Testing (.pdf)
Major airports throughout the world are equipped with Instruments Landing Systems (ILS). These systems allow the airports to operate more safely in the presence of adverse weather conditions. The complete system includes signal monitors which provide alarms to alert engineering staff should any
LXI-Based Instrumentation Connects and Synchronizes Hundreds of Data Test Points
synchronization for timing accuracies into the nanosecond range. Each time a commercial airliner, military jet, or other aircraft touches down on a runway anywhere in the world, its pilot depends on the structural integrity and mechanical stability of the landing gear to get plane and passengers down
Mars Explorer Rover
IDD during launch, travel and landing and release the. IDD when required on the planetary surface.
Huygens Probe and PAT: Exploring a New World
Operational Excellence & Lean Six Sigma New worlds require a root and branch review of our measurement techniques. The instruments on Huygens were custom-designed to ensure that they could operate reliably after the rigors of atmospheric re-entry, landing, and an environmental temperature 200Â C
More Information Top
Avionics Navigation Systems 2nd Edition Complete Document
13.5 The Instrument Landing System 608 .