AMS Performance at DC3-Test Some preliminary results Pedro Campuzano Jost, Douglas Day, Michael Lechner, Jose Luis Jimenez.

Slides:



Advertisements
Similar presentations
Research Questions How is the chemical composition* of the aerosol burden in Northern Europe modulated? –What are the chemical properties of the burden.
Advertisements

Combining the strengths of UMIST and The Victoria University of Manchester Manchester UFAM equipment at VOCALS P.I. Williams, H. Ricketts, J.R. Dorsey.
Aircraft Fire and Cabin Safety Research – Lisbon, Portugal In-Flight Fuel Tank Flammability Testing The 4th Triennial Int’l Aircraft Fire and.
PM 2.5 Carbon Measurements in EPA Region 10 Robert Kotchenruther, Ph.D. NW-AIRQUEST June, 2011.
NETCARE – POLAR Two aircraft campaigns – summer 2014, spring 2015 (spring 2016 in proposal) Close collaboration with Alfred Wegener Institute (Andreas.
Flight Instrument Systems
Optical Properties of Aerosol Particles Introduction Atmospheric aerosol particles play a significant role in determining Earth's climate, through their.
1 3 rd Integrated Seminar Cooling Tower Internals  Water pass through a nozzle  Air-water interface is heat transfer surface  Free-fall.
Some Experiments on Thermo - Acoustics of RIJKE Tube with Geometric Modifications and Forced Vorticity S.D. Sharma Aerospace Engineering Department IIT.
1 Comparison of Analog vs. Advance Technology Air Sampling System Designs To Facilitate Correction of Measured or Calculated Volumes to a Set of Reference.
Accuracy and Precision. Accuracy O refers to how close a measured or calculated value is to the correct or accepted value of the quantity measured O the.
Lecture 12 Content LIDAR 4/15/2017 GEM 3366.
HIAPER Modular Inlets (HIMIL) & Instrument Exhaust System - Dave Rogers - Outline HIMIL description contamination testing re-install HIMIL to different.
GEOS-5 Simulations of Aerosol Index and Aerosol Absorption Optical Depth with Comparison to OMI retrievals. V. Buchard, A. da Silva, P. Colarco, R. Spurr.
DIRECT TROPOSPHERIC OZONE RETRIEVALS FROM SATELLITE ULTRAVIOLET RADIANCES Alexander D. Frolov, University of Maryland Robert D. Hudson, University of.
AOSC 634 Air Sampling and Analysis Lecture 1 Measurement Theory Performance Characteristics of instruments Nomenclature and static response Copyright Brock.
Distribution of H 2 O and SO 2 in the atmosphere of Venus Yung Y. 1, Zhang X. 1, Liang M.-C. 2 and Parkinson C. 3 1 California Institute of Technology.
Atmospheric phase correction for ALMA Alison Stirling John Richer Richard Hills University of Cambridge Mark Holdaway NRAO Tucson.
D. Waddicor, G. Vaughan, K. Bower, T. Choularton, H. Coe, M. Flynn, M. Gallagher, P. Williams Aerosol observations and growth rates in the TTL.
MiniSIMS Secondary Ion Mass Spectrometer Dr Clive Jones Millbrook Instruments Limited Blackburn Technology Centre, England
Strategically Targeted Research in Intelligent Built.
MAOS (Mobile Aerosol Observing System) and the G1 Aircraft at Cape Cod Allie Marquardt Collow.
Convective Transport of Active Species in the Tropics.
Profiling Transmissivity and Contamination in Fractures Intersecting Boreholes USEPA-USGS Fractured Rock Workshop EPA Region 2 14 January 2014 Claire Tiedeman.
1 Measuring the flow boundary layer on HIAPER's fuselage Rogers, Fox, Lord, Stith, Maclean, EOL technical staff, Friehe, McClusky goal: measure air speed.
Design & Thermo Chemistry of Turbo Combustor P M V Subbarao Professor Mechanical Engineering Department Design for performance, safety and Reliability…..
Choking Pressure Ratio Guidelines for Small Critical Flow Venturis
Reason for Doing Cluster Analysis Identify similar and dissimilar aerosol monitoring sites so that we can test the ability of the Causes of Haze Assessment.
Lidar Working Group on Space-Based Winds, Snowmass, Colorado, July 17-21, 2007 A study of range resolution effects on accuracy and precision of velocity.
Federal Aviation Administration 0 Composite Wing Tank Flammability April 2-3, Composite and Aluminum Wing Tank Flammability Comparison Testing Steve.
ASSESSING INTERCONTINENTAL TRANSPORT OF OZONE AND AEROSOLS AT NORTHERN MID-LATITUDES WITH GMI Daniel J. Jacob, Rokjin J. Park, Shiliang Wu, Colette L.
LOAC (Light Optical Aerosol Counter)
Correcting TEOM Measurements using the KCL Volatile Correction Model David Green, Gary Fuller & Timothy Baker.
MELANIE FOLLETTE-COOK KEN PICKERING, PIUS LEE, RON COHEN, ALAN FRIED, ANDREW WEINHEIMER, JIM CRAWFORD, YUNHEE KIM, RICK SAYLOR IWAQFR NOVEMBER 30, 2011.
1 of 26 Characterization of Atmospheric Aerosols using Integrated Multi-Sensor Earth Observations Presented by Ratish Menon (Roll Number ) PhD.
Atmospheric Technology Division Rain In Cumulus over the Ocean Jorgen Jensen, Jeff Stith, Teresa Campos, Mary Barth, Dave Rogers NCAR science to complement.
Melanie Follette-Cook Christopher Loughner (ESSIC, UMD) Kenneth Pickering (NASA GSFC) CMAS Conference October 27-29, 2014.
A White Paper on the potential for a small scale airborne system for Threat assessment, Characterization, Monitoring, and Tactical feed-back for deployment.
AOSC 634 Air Sampling and Analysis Vertical Flux Eddy Correlation (Eddy Covariance) And Vertical Gradient Copyright Brock et al. 1984; Dickerson
HIAPER 3D Winds – current status - Dick Freisen -.
Model Evaluation Comparing Model Output to Ambient Data Christian Seigneur AER San Ramon, California.
Part II: Turbulence Signature and Platform Limitations Dan Weber, Frank W. Gallagher, Ken Howard ©2000 Frank W. Gallagher III.
Status of the P3DWL investigations on NOAA aircraft Emmitt (SWA) Atlas(AOML/NOAA) Eleuterio (ONR/USNavy) DWL WG Meeting 24 – 26 August 2010 Bar Harbor,
SEAC4RS Payload Payload Synergies Synergies. Complementarity between aircraft can be considered to fall into three categories. Each has considerations.
Federal Aviation Administration 0 Composite Wing Tank Flammability November 20, Composite and Aluminum Wing Tank Flammability Comparison Testing.
TAO buoy temp. + ASCAT. Moment of truth: composite ASCAT winds against buoy temperature; start with western equatorial Pacific. We define CPs by a temperature.
DODO RESULTS: Campaign Averages & BAe-146 Nephelometer Findings Claire McConnell Ellie Highwood Acknowledgements: Paola Formenti, Met Office, FAAM.
Relating Aerosol Mass and Optical Depth in the Southeastern U.S. C. A. Brock, N. L. Wagner, A. M. Middlebrook, T. D. Gordon, and D. M. Murphy Earth System.
Horizontal Variability In Microphysical Properties of Mixed-Phase Arctic Clouds David Brown, Michael Poellot – University of North Dakota Clouds are strong.
IASFPWG – Ottawa, Canada In-Flight Fuel Tank Flammability Testing Steve Summer Project Engineer Federal Aviation Administration Fire Safety Branch.
Combustor modeling Webinar
Jeff Stith, Andrew Gettelman NCAR is sponsored by the National Science Foundation Southern Ocean Studies: NCAR Measurement capabilities and integrating.
BBC/4DC meeting Leipzig Structure of microphysical cloud parameters in Cu and StCu clouds during the BBC/4D-Clouds field campaign at Cabauw.
Performance of a New Low-Pressure Water-Based CN Instrument - Rogers, Hering, Stolzenburg, Oberreit, Quant - Outline challenge of measuring CNchallenge.
Aerosol Chemical Speciation Monitor ACSM Instrument description and sample data N.L. Ng, T. Onasch, A. Trimborn, S. Herndon, M. Canagaratna, D. Sueper,
Data Editing Strategies Common edits Invalidation vs. contamination? What is a considered a spike? What not to edit! Automatic edits Reasons for edits.
© Crown copyright Met Office Wind and turbulence measurements on the BAe146 Phil Brown, OBR Conference, Dec 2012.
PHOTOTUBE SCANNING SETUP AT THE UNIVERSITY OF MARYLAND Doug Roberts U of Maryland, College Park.
Challenges associated with ice and large particles in the TTL
Submicron Aerosol Composition by the CU-HR-AMS
Session 4: Air Pollution Measurements
A LATENT HEAT RETRIEVAL IN A RAPIDLY INTENSIFYING HURRICANE
August 23, 2000 R.N. Dubois Dow Chemical
Alberto Sánchez-Marroquín, S. T. Parker, J. Trembath, I. Burke, J. B
Lemnos 11/9/03 Comparison of PM exhaust emissions measured at a chassis dynamometer and on-road chasing on a test track.
Characterization of Inlet Contamination Potential
ICHS5 – 2013 September, Brussels, Belgium | ID161
Mosquitoes Use Vision to Associate Odor Plumes with Thermal Targets
Longer Term Aerosol Chemical speciation monitoring data during ACTRIS/EMEP activities ACSM Teams across Europe Many slides from Michael Bressi, JRC Italy.
Measurement Needs for AQ Models
Presentation transcript:

AMS Performance at DC3-Test Some preliminary results Pedro Campuzano Jost, Douglas Day, Michael Lechner, Jose Luis Jimenez

Overview Instrument was in working order for all six flights. Data was acquired for >95% of flight time (the rest being filters and software mode switches). Real time data was exported for all six flights to the G-V data system. After some minor software fixes, starting with RF03 the stream was fully functional Topics Inlet characterization: Still loose ends, but basic performance seems acceptable UHSAS comparison Stratospheric/UT aerosol measurements in clean air and after deep convection: AMS detection limit Sampling of polluted air thru clouds: AMS time resolution Size and chemical characterization of organics: brief case study

Inlet A new secondary diffuser was build for improved sampling of larger particles. At the same time, small modifications were performed on the pressure controlled inlet (PCI) system to make it work all the way to ft The transmission of the PCI showed little changes in transmission over a wide range of inlet flows, being close to 100% for submicron aerosol To characterize the transmission of the inlet system up to the AMS, the following was investigated: Flow into the system under “free flow” conditions. Is the diffuser working? Is the pressure drop sufficient despite the filters to run the inlet? Comparison of concentrations and size distributions for free flow and “choked” flow thru rapid switches Comparison with calculated inlet transmissions Comparison with the UHSAS (RF02 and 03)

Aircraft Speed vs Inlet Velocity, “free flow” conditions RF01RF02RF03 RF06 RF05 RF04 Red: Scaled Airspeed Black: Cabin flow speed Green: Corrected inlet speed, free flow Blue: Scaled airspeed x 1.4

Aircraft Speed/Inlet Velocity vs Height, “free flow” conditions (actual ratios) RF01RF02RF03 RF06 RF05 RF04 Red Line: “Ideal ratio”. Bottom range: kft

Varying Inlet speeds (free, /2, /4) during RF05: Nitrate

Varying Inlet speeds (free, /2, /4) during RF05: Sulfate Only for low to midheights! Testing during RF06 for >40 kft showed the same (s.b.)

Chemically Resolved Size Distributions during the switching

Size Distributions during the switch (averages)

Calculated trasmission(line only) “Free flow” “Free Flow”/2

UHSAS comparison, RF02 Filter

UHSAS Comparison, RF03

Altitude Profiles (RF01, RF03)

Altitude Profiles (RF05, RF06)

Stratosphere/UT aerosol loadings This is a switched dataset!

Typical AMS Detection Limits

AMS Response to fast changing conditions Missed Approaches I: COS

Missed Approaches I: COS (detail)

Speeding thru clouds on the way to COS (10 kft)…

Missed Approaches II: BJC Cloud base higher than COS, hence no sharp transitions as seen there. The “sulfate mystery spike” still shows up here, though

Speciated Mass Size Distributions

Bloomfield metro vs RM Nat Park

Things to do for DC3-test… CFD modeling of the inlet in collaboration with RAF (Dave Rogers) would be very helpful to understand the exact behavior at high altitude and under high pitch and roll angles (would be extremely useful for all aerosol instruments in the HIAPER cabin). Explore HR analysis and repeat UHSAS comparison according to Middlebrook et al, 2011 Take a closer look at the mass spectral signature of the organic aerosol measured in the stratosphere during RF06 Once available, explore correlations between AMS loadings with the other chemical data acquired during DC-3 Try to increase the data quality of the size distributions by developing an HR analysis procedure for them

Things to do before the next campaign (RHINO 2014?) Depending on funding integrate cryopump to reduce pre- flight pumping requirements and increase sensitivity. Automate filter sampling. Redesign inlet assembly for easier service Add flow meter to PCI bypass flow line Explore software options for remote control of the AMS Fly with a heated HIMIL and temperature monitor next time.