NCAR/NSF GV New Automated Dropsonde System Overview
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1 NCAR/NSF GV New Automated Dropsonde System Overview MPEX Meeting 13 December 2012 National Center for Atmospheric Research Earth Observing Lab Boulder, CO Terry Hock GV Dropsonde Team ISF - Terry Hock, Dean Lauritsen, Nick Potts, Clayton Ardent, Chip Owens DFS - Jim Ranson, Cindy Bradley RAF - Steve Raumbuler, Mark Lord, Kurt Zrubek, Chris Webster CDS - Charlie Martin, Xuanyong Xu, FPS -Brigitte Baeuerle 5 EOL Facilities 1
2 NCAR Dropsonde Technology Complete end to end solution Dropsondes Aircraft Data Systems Atmospheric Profiling Research quality sensors Fast sample rate- high vertical resolution - Pressure - Temperature - Humidity - Winds Capability of rapid launch, up to 8 sondes in the air simultaneously. Launch Platforms - Manned Aircraft Systems - Global Hawk UAS - Long duration balloons (Driftsonde ) 2012 Copyright University Corporation for Atmospheric Research ASPEN Software Data Quality and Temp Drop message Automatic launcher
3 G-V Design Criteria for New System Technology developed for the NASA Global Hawk applied to the NSF/NCAR G-V System Curtain of sondes every ~15km (rapid deployment up to 8 sondes) Operator safety Mini Dropsonde (<6oz) Automatic Launcher Capacity: 50 Mini Dropsondes Flight path Drop in turbulence Optional dedicated Dropsonde operator Ability to reload launcher during flight No flight limitations Remote Operation 3
4 Summary of Capabilities Automated launcher No flight restrictions to operator thus no limiting criteria for drops during flight. Automated sonde prep/sounding Rapid Launches Remote operation via AGS software Total Number of dropsonde in air simultaneously Dropsonde New GV Dropsonde System 2-button operation ~ 2 minute Multiple seat locations on G-V 8 Channel System Mini Dropsonde (167 grams) Dropsondes capacity /flight Launcher located in baggage compartment FAA Certification 4
5 GV Dropsonde System Overview Ground Operations AGS ASPEN AVAPS Flight/Ground System (AFGS) AVAPS Operator Station SatCom to Ground (Inmarsat/Iridium) ADS Ethernet AVAPS System Computer & Monitor AVAPS Sounding Software AGS Software Ethernet Sonde Storage Container & Launcher (GV Baggage Compartment) Dropsonde Automated Launcher 50 Sonde capacity Ground Command & Control, Data Display, Field Catalog AFGS Display Computer AGS AEROS Ethernet Ethernet 8-channel Telemetry Chassis AFGS Display Computer AGS AEROS Pilot Launch Enable/Disable (Cockpit) 5
6 Sonde Storage & Ejection System Launcher all designed by EOL DFS & RAF Manufactured by DFS Machine Shop
7 New GV Automated Launcher Sonde Storage Container 5 columns of 10 sondes each Capacity 50 Mini Dropsondes Launcher Control Electronics Sonde Ejection System Launch Tube Automatic Gate valves Ejection Air supply 7
8 Dropsonde Storage System Sonde Storage Capacity: 50 sondes Sonde storage can be reloaded during flight Sonde Carriage unit Loads sonde into Ejections System 8
9 Sounding Time Line Task Time Location Initialize & load sonde for launch 2 minutes G-V Aircraft Dropsonde Fall Time ~15 45,000 ft. G-V Aircraft Data transfer at completion of drop ~3 minutes G-V Aircraft ASPEN Processing minutes Ground Ops Center Process data by student? Ground Ops Center Send data to GTS Ground Ops Center Send data files to Field Catalog Total Time per Sounding minutes per drop Ground Ops Center 2012 Copyright University Corporation for Atmospheric Research 9
10 Operational Remote Software AVAPS Ground Software (AGS) Button Sounding Interface 1) Load sonde 2) Launch sonde AGS on any computer Flight Computers Ground Computers System does not need dedicated Dropsonde operator Remote interface will be via the existing datagram protocol developed for the Global Hawk deployment. Data feeds will integrate into the existing Aeros database structure and display. Pilot over-ride for launch. 10
11 NCAR GPS Dropsondes ( MIST, Mini, AVAPS II/Vaisala RD-94 ) Research quality measurements Pressure Temperate Humidity Winds speed/direction High vertical resolution Multiple sonde in air simultaneously Performance Specs Fall speed ~11 m/s at sea surface Fall Time: ~15 Min from 45K ft. PTU Sensors Measurement rate every 500 msec (Vaisala RS-92 PTU module) Vertical resolution : ~ 6 surface Pressure 0.1 mb resolution 0.5 mb repeatability Temperature 0.1 resolution 0.2 repeatability Humidity 1% resolution 2% repeatability Winds Measurement rate every 250 msec Horizontal Winds 0.1 m/s resolution Vertical resolution : ~ 3 surface Stable parachute design AVAPS II Mini Mini sonde Size: Mass: 165 grams Length: 30.5 cm Diameter: 4.7 cm AVAPS II Sonde Size: Mass: 320 grams Length: 40.6 cm Diameter: 7 cm 11
12 NCAR Mini Dropsonde (Same sonde used on NASA Global Hawk) Hurricane Leslie from NASA AV-6 Global Hawk Raw Data Plot, no Quality Control 12
13 Drop Altitude (Feet) Sonde Fall Time 60,000 Fall Time vs Altitude 50,000 40,000 30,000 20,000 10, Fall Time (minutes) 2012 Copyright University Corporation for Atmospheric Research 13
14 Altitude (feet) Sonde Fall Velocity 50,000 45,000 40,000 35,000 30,000 25,000 20,000 15,000 10,000 5,000 0 Descent Velocity vs Altitude 27 m/s 15 m/s 12 m/s 2,000 2,500 3,000 3,500 4,000 4,500 5,000 5,500 6,000 Vertical Velocity (ft/min) 2012 Copyright University Corporation for Atmospheric Research 14
15 Horizontal Distance traveled between Launch & impact Locations Mini sondes released from Global Hawk during WISAR ( Altitude range adjusted from 48,000 ft. to sea level ) 2012 Copyright University Corporation for Atmospheric Research 15
16 MPEX Soundings Data Flow NCAR/NSF G-V Aircraft AVAPS Raw Sonde Data Dropsonde AVAPS D_P Sounding Data Files Satellite Link MPEX Ground Ops Center ASPEN Processing ASPEN Processed TEMP DROP Sounding Data Files ASPEN Processed EOL Sounding Data Files AGS Monitor Data & System Real-time GTS Temp Drop Message ASPEN Synoptic Plots Graphics ASPEN Skew-T Plots Field Data Catalog Graphics ASPEN Processed Sounding Data Files Preliminary Data Files
17 ASPEN- Tabular QC ed Data 2012 Copyright University Corporation for Atmospheric Research 17 Aspen-3
18 2012 Copyright University Corporation for Atmospheric Research 18 Aspen-4 ASPEN X-Y Data Plot Wind Speed & Direction
19 ASPEN Skew-T Plot 2012 Copyright University Corporation for Atmospheric Research 19 Aspen-5
20 ASPEN Temp Drop Significant and Mandatory Levels 2012 Copyright University Corporation for Atmospheric Research 20 Aspen-6
21 Hurricane Sandy 2012 Copyright University Corporation for Atmospheric Research 21
22 Hurricane Sandy NOAA/AOC Drops ASPEN Synoptic Plot 850 mb Level 2012 Copyright University Corporation for Atmospheric Research 22
23 G-V Dropsonde Project Project Management & Documentation System is based upon the Global Hawk System NASA HS3 2011, NASA HS3 2012, NOAA WISPAR Dedicated Project Manager Project Charter Document Technical Requirements Document Gantt Chart / Project Time Line Timeline July 2011 March 2013 (21 months) EOL Staff FTE: ~4.5 yrs (Techs, Eng, Mechanics, Management) Current Schedule & Status Completion of Sonde storage and Ejection Assembly Oct 2012 Core Software Development June to Dec 2012 Lab System Testing and preliminary G-V Integration Nov to Dec 2012 GV Installation and ground aircraft testing Jan 2013 Flight Tests Feb 2013 First Deployment - May - June 2013 MESOSCALE PREDICTABILITY EXPERIMENT (MPEX) 23
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