7760, 2276, 2248, 6240C-10, 6240M10 MEASUREMENT IN LOW TEMPERATURE ENVIRONMENTS Measurements performed near cryogenic conditions, such as cooling systems on rocket engines or space- craft components, require transducers that can operate at temperatures near absolute zero. Most accelerometer designs

176;F 2276 SE 100 kΩ at 900°F 2280 SE 100 kΩ at 900°F 6222S Diff 50 MΩ at 500°F 6233C Diff 100 kΩ at 900°F 6237M70 SE 10 kΩ at 1200°F 6243M1 SE 10 kΩ at 1200°F 6243M3 Diff 10 kΩ at 1200°F Table 1 [Source: Ref 1] Considerations for using charge amplifiers with high