SOW.pdf
PDF 224 KB Posted
- Attached to
- Rack Mounted Twin Channel Laboratory ADTS Federal contract opportunity
- Solicitation number
- 80NSSC25913078Q
About this file
This document presents Minimum Technical Requirements for an Air Data Controller, specifying detailed technical specifications for a sophisticated pressure measurement device. The requirements include two independent absolute pressure transducers capable of measuring static and total pressures across extreme altitude and speed ranges (from 100,000 ft. altitude to 36 inHga, and speeds up to 900 knots). The device must be RVSM compliant, multi-gas species capable (minimum GN2 and Air), and able to pressurize and control a 5187 cu. in./87-liter volume with demonstrated stability. Additional technical requirements include IEEE-488 bus SCPI for automated operation, UUT head correction input, owner-enabled in-house calibration capabilities, and a 19" rack mountable design to facilitate integration into existing systems.
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Text version
Minimum Technical Requirements for Air Data Controller
Two independent absolute pressure transducers, Ps and Pt (Qc derived)
Aeronautic and engineering units, including psia (Ps,Pt), psid (Qc) and User Defined
Ps > 100,000 ft. alt. to minimum 36 inHga, Pt < 1.0 inHga, to > 900 kts / 50 inHga
Capable of concurrent independent Measure/Control of Ps/Pt
RVSM Compliant
Multi-gas species capable, minimum GN2 and Air
Must pressurize and control with stability a 5187 cu. In. / 87-liter volume and provide documentation demonstrating this capability (such as testing output results)
UUT head correction input
IEEE-488 bus SCPI for automated operation
Provide for in-house Ps/Pt calibration by owner
Must be 19” rack mountable
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