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Customer Proposal 17-10397 <br />2.0 TECHNICAL SUMMARY Exhibit 3 <br />2.1 DESIGN CONDITIONS <br />PROCESS DATA <br />GAS COMPOSITION <br />MAX FLOW RATE <br />RATED HEAT RELEASE PER HTF UNIT <br />INLET TEMPERATURE: <br />INLET PRESSURE: <br />RETENTION TIME: <br />DESTRUCTION RATE EFFICIENCY: <br />OPERATING TEMPERATURE: <br />NOX EMISSIONS REQUIREMENT: <br />CO EMISSIONS REQUIREMENT: <br />2.2 SITE CONDITIONS <br />56.9% CH4 and 43.1% AIR <br />2.86 MMSCFD <br />62 MMBTU/HR <br />100'F MAX <br />30 PSIG <br />MINIMUM 0.3 SEC <br />99.9% DRE <br />UP TO 1,800 °F <br />0.15 LBS/MM BTU <br />0.2755 LBS/M M BTU <br />AMBIENT TEMPERATURE: 30 — 100 °F <br />WIND SPEED FOR STRUCTURAL CALCULATIONS: TBD <br />SEISMIC CLASSIFICATION: TBD <br />ELEVATION (ABOVE MEAN SEA LEVEL): TBD <br />2.3 UTILITIES <br />PILOT GAS: IF NATURAL GAS IS USED: 65 SCFH @ 10 PSIG (PER IGNITOR) <br />ELECTRICAL: 1 PHASE, 60 HZ, 120VAC <br />ELECTRICAL AREA CLASSIFICATION CLASS 1 DIV. 2 <br />INSTRUMENT AIR: N/A <br />61 <br />AEREON.COM <br />