Photos of the ACES II seat…

02.09.2023

Here’s a link to some photos I took of the seat right after I got it “unboxed”.

ACES II Ejection Seat – Prior to restoration.

This page can also be found on the Technical tab above.

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F-15 Instrumentation Resolution and Sampling Rates

09.11.2013
Parameter Name Source Range Resolution Samples Per Second
Left Aileron Position Transducer +/- 20 deg 0.05 deg 53.33
Right Aileron Position Transducer +/- 20 deg 0.05 deg 53.33
Left Stabilator Position Bus – 16 bit -30deg to +15 deg 0.006 deg 26.66
Right Stabilator Position Bus – 16 bit -30deg to +15 deg 0.006 deg 26.66
Left Rudder Position Transducer +/- 3 0deg 0.04 deg 53.33
Right Rudder Position Transducer +/- 30 deg 0.04deg 53.33
Speed Brake Position Transducer 0 to 45 deg 0.03 deg 53.33
Longitudinal Stick Force Transducer +/- 25lbs 0.04lbs 53.33
Lateral Stick Force Transducer +/- 20lbs 0.05lbs 53.33
Longitudinal Stick Position Transducer -3 to 6in 0.008in 53.33
Lateral Stick Position Transducer +/- 4in 0.007in 53.33
Right Rudder Pedal Force Transducer +/- 200lbs 0.3lbs 53.33
Left Rudder Pedal Force Transducer +/- 200lbs 0.3lbs 53.33
Right Rudder Pedal Position Transducer +/- 4in 0.02in 53.33
Left Rudder Pedal Position Transducer +/- 4in 0.02in 53.33
Right Power Lever Angle Transducer 0deg to 130deg 0.09deg 6.66
Left Power Lever Angle Transducer 0deg to 130deg 0.09deg 6.66
Left Fuel Flow Transducer 0 to 100,000 lbs/hr 0.024 lbs/hr 6.66
Right Fuel Flow Transducer 0 to 100,000 lbs/hr 0.024 lbs/hr 6.66
Left Fuel Flow Transducer 0 to 100,000 lbs/hr 0.024 lbs/hr 6.66
Left Engine Nozzle Area Transducer 2.5 to 65 sqft 0.022 sqft 6.66
Right Engine Nozzle Area Transducer 2.5 to 65 sqft 0.022 sqft 6.66
Left Core Speed (N2) Production System 0 to 110% 0.2% 53.33
Right Core Speed (N2) Production System 0 to 110% 0.2% 53.33
Pressure Altitude Bus – 16 bit -1,560 to 80,337ft 1.25ft 26.66

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