GAP Measurements and Instrumentation

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Presentation transcript:

GAP Measurements and Instrumentation Aircraft navigation Position GPS Meteorology Air temperature, pressure, humidity Wind speed and direction Updraft velocity Vaisala sensor Turbulent gust probe Radiometers Total downwelling solar irradiance (0.200 to 3.6 mm) Cloud and surface albedo (reflected solar irradiance) Multi-channel downwelling irradiance (405, 550, 875 nm, PAR) Transmitted solar radiation and cloud optical depth modified CM22 pyranometer (Kipp & Zonen) modified CM22 pyranometer (Kipp & Zonen) and Multi-Channel Airborne Radiometer (MCAR-4) (Biospherical Instruments, Inc.) MCAR-4 (Biospherical Instruments) MCAR-4 (Biospherical Instruments, Inc.) Cloud and aerosol measurements Condensation nuclei concentration Cloud condensation nuclei (0.13 to 3% S) Aerosol size distribution (0.3 to 10 mm Dp) Cloud droplet distribution (1 to 70 mm Dp) Cloud liquid water content Cloud imaging Rain drop and drizzle size distribution Condensation particle counter (CPC) (TSI 3007) CCN counter (Scripps / Georgia Tech / DMT) Optical particle counter (MetOne) Cloud droplet probe (CDP) (DMT) infer from CDP (in-situ; future development) Video camera 2D Probe (DMT; future development) Gas measurements CO CO2 SO2 Volatile organic carbon compounds (future development)

GAP Instruments (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 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 Flow Splitter / Inlet (AI) NOTE: fuselage part of aerosol inlet Additional: Electronics processor for CDP Pressure sensors for GP

GAP Instruments (external) 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 Pyranometer (CM22-A) Weight: 0.4 kg Dimensions: 80 x 55 x 70 mm Power consumption: NA Data output: RS-232 Deployment: wing 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

Deployment of GAP Instruments ID Est. weight (kg) Power (W) Data acquisition Condensation Particle Counter CPC 0.75 15.0 RS-232 Optical Particle Counter OPC 0.30 5.4 Cloud Droplet Probe CDP 1.6 14.0 Pyranometer CM22-A 0.40 NA datalogger Multi-Channel Airborne Radiometer (405, 550, 875, PAR) MCAR 0.1 Cloud Condensation Nucleus Counter CCN 3.00 25.0 digital video camera DC 0.5 Flash card data acquisition system DAQ 10 -- aerosol inlet AI 0.3 Estimated payload for each platform Payload (kg) Instrumentation above-cloud 3.75 30.7 AI, DAQ, CPC, 2*CM22, OPC, 2*MCAR, DC in-cloud 3.85 45.4 AI, DAQ, CPC, CDP, OPC below-cloud 4.85 50.1 AI, DAQ, CPC, CCN, MCAR, OPC

GAP-PT Instrumentation 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 Platform specific instruments Pyranometer (CM22-A) Weight: 0.4 kg Dimensions: 80 x 55 x 70 mm Power consumption: NA Data output: RS-232 Deployment: wing 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 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 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 Platform specific instruments Pyranometer (CM22-A) Weight: 0.4 kg Dimensions: 80 x 55 x 70 mm Power consumption: NA Data output: RS-232 Deployment: wing 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 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 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 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 in-cloud instrumentation 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 Platform specific instruments 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 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 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 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 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 Additional: Electronics processor for CDP Pressure sensors for GP

GAP-FM1 below-cloud instrumentation 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 Platform specific instruments 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 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 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 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 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 Additional: Pressure sensors for GP