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Taber Aerospace Transducers Model 2403SAT0 pages
نسخه متنی
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| Pressure Transducer | |||||||||
| Bonded Foil Sensing Technology | |||||||||
| Designed Using Advanced Computer Modeling Tools For optimum performance, the sensing element was designed using Finite Element Analysis and other computer modeling tools. Key features of the sensing element are isolation from induced stresses (generated from installation torque, temperature excursions, vibration and shock), and high over-pressure protection. | |||||||||
| Manufactured for Aerospace Grade Applications Reliability and accuracy are built into every transducer using advanced manufacturing techniques. Critical procedures such as heat-treat and bonding are controlled through vacuum furnaces. Welding and calibration are accomplished with fully automated work cells. State of the art characterizing electronics meet MIL-STD 461 EMI standards, and are engineered for severe vibration and shock environments. Extreme environmental burn-in ensures the transducer's reliability and accuracy will be maintained over time. | |||||||||
| Class S, Class B, or MIL-STD Electronics High reliability electronic components are available to meet the most stringent flight requirements. Providing a choice of selections permits cost optimization while meeting program life needs. | |||||||||
| Standard and Customer Configurations Available The Model 2403SAT was designed for the smaller satellites based on the heritage and success of the Model 2403. Materials of construction, mechanical and electrical interfaces are selected for reliability and ease of installation. Standard and custom test programs are offered. | |||||||||
| Standard Features 0-50 thru 0-5000 psi Class B high reliable electronics +/- 0.1% FSO per annum long term stability | |||||||||
