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GAP Measurements and Instrumentation

GAP Measurements and Instrumentation. Optical Particle Counter (OPC) Weight: 0.30 kg Dimensions: 96 x 60 x 34 mm Power consumption: 5.4 W (12 V DC) Data output: RS-232 Deployment: fuselage. Condensation Particle Counter (CPC) Weight: 0.75 kg Dimensions: 250 x 120 x 70 mm

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GAP Measurements and Instrumentation

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  1. GAP Measurements and Instrumentation

  2. Optical Particle Counter (OPC) Weight: 0.30 kg Dimensions: 96 x 60 x 34 mm Power consumption: 5.4 W (12 V DC) Data output: RS-232 Deployment: fuselage Condensation Particle Counter (CPC) Weight: 0.75 kg Dimensions: 250 x 120 x 70 mm Power consumption: 15 W (9 VDC) Data output: RS-232 Deployment: fuselage Cloud Condensation Nuclei Counter (CCN) Weight: 3 kg Dimensions: ca. 120 x 120 x 300 mm Power consumption: 25 W (28 VDC) Data output: RS-232 Deployment: fuselage Flow Splitter / Inlet (AI) NOTE: fuselage part of aerosol inlet Data Acquisition (DAQ) Weight: 0.08 kg Dimensions: ca 100 x 100 x 15 mm Power consumption: 5 W (5 V DC) Data output: RS-232 Deployment: fuselage GAP Instruments (fuselage) Additional: Electronics processor for CDP Pressure sensors for GP

  3. Pyranometer (CM22-A) Weight: 0.4 kg Dimensions: 80 x 55 x 70 mm Power consumption: NA Data output: RS-232 Deployment: wing Cloud Droplet Spectrometer (CDP) Weight: 1.6 kg Dimensions: 216 x 115 x 100 mm Power consumption: 14 W (28 V DC) Data output: datalogger Deployment: fuselage/wing NOTE: electronics processor in fuselage Multi-Channel Airborne Radiometer (MCAR-4) Weight: 0.3 kg Dimensions: 90 mm  x 110 mm Power consumption: ~10 mA (RS-232) Data output: RS-232 Deployment: wing or fuselage Gust Probe (GP) Weight: 0.4 kg Dimensions: 6 Ø x 200 mm Power consumption: < 1 W Data output: datalogger Deployment: nose NOTE: ca. 0.1 liters of sensors in fuselage Aerosol Inlet (AI) Weight: 0.3 kg Dimensions: 30 Ø x 200 mm Power consumption: NA Data output: NA Deployment: nose NOTE: splitter in fuselage GAP Instruments (external)

  4. Deployment of GAP Instruments

  5. Optical Particle Counter (OPC) Weight: 0.30 kg Dimensions: 96 x 60 x 34 mm Power consumption: 5.4 W (12 V DC) Data output: RS-232 Deployment: fuselage Pyranometer (CM22-A) Weight: 0.4 kg Dimensions: 80 x 55 x 70 mm Power consumption: NA Data output: RS-232 Deployment: wing Data Acquisition (DAQ) Weight: 0.08 kg Dimensions: ca 100 x 100 x 15 mm Power consumption: 5 W (5 V DC) Data output: RS-232 Deployment: fuselage Condensation Particle Counter (CPC) Weight: 0.75 kg Dimensions: 250 x 120 x 70 mm Power consumption: 15 W (9 VDC) Data output: RS-232 Deployment: fuselage Aerosol Inlet (AI) Weight: 0.3 kg Dimensions: 30 Ø x 200 mm Power consumption: NA Data output: NA Deployment: nose NOTE: splitter in fuselage Flow Splitter / Inlet (AI) NOTE: fuselage part of aerosol inlet GAP-PT Instrumentation Platform specific instruments

  6. Optical Particle Counter (OPC) Weight: 0.30 kg Dimensions: 96 x 60 x 34 mm Power consumption: 5.4 W (12 V DC) Data output: RS-232 Deployment: fuselage Pyranometer (CM22-A) Weight: 0.4 kg Dimensions: 80 x 55 x 70 mm Power consumption: NA Data output: RS-232 Deployment: wing Data Acquisition (DAQ) Weight: 0.08 kg Dimensions: ca 100 x 100 x 15 mm Power consumption: 5 W (5 V DC) Data output: RS-232 Deployment: fuselage Condensation Particle Counter (CPC) Weight: 0.75 kg Dimensions: 250 x 120 x 70 mm Power consumption: 15 W (9 VDC) Data output: RS-232 Deployment: fuselage Multi-Channel Airborne Radiometer (MCAR-4) Weight: 0.3 kg Dimensions: 90 mm  x 110 mm Power consumption: ~10 mA (RS-232) Data output: RS-232 Deployment: wing or fuselage Aerosol Inlet (AI) Weight: 0.3 kg Dimensions: 30 Ø x 200 mm Power consumption: NA Data output: NA Deployment: nose NOTE: splitter in fuselage Flow Splitter / Inlet (AI) NOTE: fuselage part of aerosol inlet GAP-FM1 above-cloud instrumentation Platform specific instruments

  7. Optical Particle Counter (OPC) Weight: 0.30 kg Dimensions: 96 x 60 x 34 mm Power consumption: 5.4 W (12 V DC) Data output: RS-232 Deployment: fuselage Data Acquisition (DAQ) Weight: 0.08 kg Dimensions: ca 100 x 100 x 15 mm Power consumption: 5 W (5 V DC) Data output: RS-232 Deployment: fuselage Cloud Droplet Spectrometer (CDP) Weight: 1.6 kg Dimensions: 216 x 115 x 100 mm Power consumption: 14 W (28 V DC) Data output: datalogger Deployment: fuselage/wing NOTE: electronics processor in fuselage Condensation Particle Counter (CPC) Weight: 0.75 kg Dimensions: 250 x 120 x 70 mm Power consumption: 15 W (9 VDC) Data output: RS-232 Deployment: fuselage Gust Probe (GP) Weight: 0.4 kg Dimensions: 6 Ø x 200 mm Power consumption: < 1 W Data output: datalogger Deployment: nose NOTE: ca. 0.1 liters of sensors in fuselage Aerosol Inlet (AI) Weight: 0.3 kg Dimensions: 30 Ø x 200 mm Power consumption: NA Data output: NA Deployment: nose NOTE: splitter in fuselage MAY REQIURE REVERSE FACING INLET Flow Splitter / Inlet (AI) NOTE: fuselage part of aerosol inlet GAP-FM1 in-cloud instrumentation Platform specific instruments Additional: Electronics processor for CDP Pressure sensors for GP

  8. Optical Particle Counter (OPC) Weight: 0.30 kg Dimensions: 96 x 60 x 34 mm Power consumption: 5.4 W (12 V DC) Data output: RS-232 Deployment: fuselage Data Acquisition (DAQ) Weight: 0.08 kg Dimensions: ca 100 x 100 x 15 mm Power consumption: 5 W (5 V DC) Data output: RS-232 Deployment: fuselage Condensation Particle Counter (CPC) Weight: 0.75 kg Dimensions: 250 x 120 x 70 mm Power consumption: 15 W (9 VDC) Data output: RS-232 Deployment: fuselage Cloud Condensation Nuclei Counter (CCN) Weight: 3 kg Dimensions: ca. 120 x 120 x 300 mm Power consumption: 25 W (28 VDC) Data output: RS-232 Deployment: fuselage Multi-Channel Airborne Radiometer (MCAR-4) Weight: 0.3 kg Dimensions: 90 mm  x 110 mm Power consumption: ~10 mA (RS-232) Data output: RS-232 Deployment: wing or fuselage Gust Probe (GP) Weight: 0.4 kg Dimensions: 6 Ø x 200 mm Power consumption: < 1 W Data output: datalogger Deployment: nose NOTE: ca. 0.1 liters of sensors in fuselage Aerosol Inlet (AI) Weight: 0.3 kg Dimensions: 30 Ø x 200 mm Power consumption: NA Data output: NA Deployment: nose NOTE: splitter in fuselage Flow Splitter / Inlet (AI) NOTE: fuselage part of aerosol inlet GAP-FM1 below-cloud instrumentation Platform specific instruments Additional: Pressure sensors for GP

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