1 / 8

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

michaelerickson
Download Presentation

GAP Measurements and Instrumentation

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  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

More Related