The Atmospheric Chemistry Experiment (ACE)

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    The Atmospheric Chemistry

    Experiment (ACE)

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    ACE Primary Science GoalTo investigate the chemical and dynamical

    processes that control the distribution of ozone inthe stratosphere and upper troposphere with a

    particular focus on the Arctic winter stratosphere.

    To accomplish this,

    Temperature and pressure will be measured.

    ACE will measure the concentrations of more than

    30 molecules as a function of altitude.

    Aerosols will be measured and quantified.

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    Atmospheric Structure

    O2 + h 2O*

    2O* + 2O2 2O3*

    UV photon

    Excess energy goes

    into thermal motion

    of molecules.

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    Volume Mixing Ratio

    Ratio of gas partial pressure to total pressure.

    Variation with altitude gives information on

    chemical or photochemical processes

    Ozone Vmr Profile

    0

    20

    40

    60

    80

    100

    120

    0 2 4 6 8 10

    vmr (parts per million by volume)

    Altitude(km)

    CO2 Vmr Profile

    0

    20

    40

    60

    80

    100

    120

    100 150 200 250 300 350 400

    vmr (parts per million by volume)

    Altitude(km

    )

    CO Vmr Profile

    0

    20

    40

    60

    80

    100

    120

    0 50 100 150 200

    vmr (parts per million by volume)

    Altitude(km)

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    Chlorofluorocarbons (CFCs)

    Cl + O3 ClO + O2

    ClO + O Cl + O2

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    Stratospheric Chlorine The long lifetimes of CFCs led to increasing

    Cl into the stratosphere (a very bad thing).

    Eventually the Cl gets taken up in reservoir

    molecules such as HCl and ClONO2.e.g., ClO + NO2 + M ClONO2 + M

    However, atomic Cl can be released in large

    quantities as a result of processes that occur

    during polar winter, leading to ozone losses.

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    Ozone Hole (continued) Temperature inside the polar vortex gets

    very cold. For temperatures below -80 C,clouds composed primarily of HNO3 (polar

    stratospheric clouds or PSCs) form.

    Reactions that occur slowly (or not at all) in

    gas phase readily proceed on the surface of

    PSC particles (heterogeneous reactions).e.g., HCl + ClONO2 HNO3 + Cl2

    HNO3 remains in cloud particle, while Cl2 is

    released into the stratosphere.

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    Ozone Hole (continued) No sunlight reaches the South Polar

    stratosphere during the winter.

    When sunlight returns in the spring, Cl2 is

    photolysed into Cl atoms. Rampant ozone destruction ensues.

    HNO3 tied up in PSC particles. Low

    nitrogen and hydrogen levels slows thecreation of chlorine reservoir molecules,

    exacerbating the destruction.

    Recovery after polar vortex breakdown.

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    Antarctic Ozone

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    Fixing the Problem Montreal Protocol signed in 1987 to phase out

    the use of CFCs.

    CFC replacements hydrofluorocarbons (HFCs)

    and hydrochlorofluorocarbons (HCFCs). HFCs contain no chlorine.

    HCFCs are much more reactive than CFCs.

    They undergo reactions in the troposphere thatcan remove them (e.g., conversion to water

    soluble species that get rained out).

    Less Cl transported to the stratosphere.

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    HCl and ClONO2 Trends

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    Role of ACE Investigate PSCs, particularly composition.

    Monitor stratospheric chlorine levels.

    Monitor CFCs and CFC replacements.

    Monitor molecules associated with polarspring chemistry (e.g., ClO and ClONO2),

    particularly at altitudes where PSCs are

    present.

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    Arctic Ozone No ozone hole occurs in the Arctic.

    Arctic winter temperatures are not as cold

    as for Antarctic winter. The polar vortex is

    also less stable in the Arctic. However, sharp declines in ozone levels

    are often observed during March/April

    (spring in the Northern Hemisphere). The reasons for the declines are similar to

    the cause of the Antarctic ozone hole

    (chlorine activation via PSCs).

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    Polar Spring Ozone

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    Mid-Latitude Ozone Decline

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    Mid-Latitudes Declines at mid-latitudes arise from a variety

    of sources: CFCs, mixing of ozone-depletedair from polar spring events, heterogeneous

    reactions on aerosol particles.

    The extent of the losses cannot be explained

    by current models.

    Most recent mid-latitude measurementsindicate that the losses have leveled off, likely

    related to the peaking of chlorine levels.

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    Chemistry-Climate Coupling A model predicts there may be an Arctic

    ozone hole in the 2010-2020 timeframe.

    Chlorine levels are decreasing, but

    greenhouse gas (e.g., CO2, CH4, N2O)levels are increasing.

    Greenhouse gases warm the surface but

    lead to a cooling of the stratosphere. A colder Arctic polar winter stratosphere

    would lead to a more stable polar vortex

    and more PSCs more ozone loss.

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    Arctic Ozone Predictions

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    Data Assimilation More reliable model predictions are needed

    for the future of Arctic ozone. Long leadtimes would be required to implement policy

    changes for greenhouse gas reductions.

    ACE measurements (and other satellite

    mission measurements and airplane- and

    balloon- and ground-based data) needs tobe assimilated into models to improve the

    reliability of the predictions.

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    ACE Satellite

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    Instruments Infrared Fourier Transform Spectrometer

    operating between 750 and 4100 cm-1

    witha resolution of 0.02 cm-1.

    2-channel visible/near infrared Imagers,

    operating at 0.525 and 1.02 microns Suntracker keeps the instruments pointed

    at the suns radiometric center.

    UV / Visible spectrometer (MAESTRO)

    0.285 to 1.03 microns, resolution ~1-2 nm

    Startracker

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    ACE Payload

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    ACE-FTS

    MAESTRO (Fli ht M d l)

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    MAESTRO (Flight Model)

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    Optical Layout (Bomem)

    Seconday

    mirror (6)

    Field stop (5)

    IR Filter

    (7)

    Suntrackermirror (1)

    Aperture

    stop (4)

    PV MCT

    Detector

    (18)

    Glare stop(16)

    Coolerwindow (17)

    Output

    condenser

    (14)

    INTcorner-cube

    mirror (10)

    End mirror

    (13)

    INT

    corner-cubemirror (11)

    (12)

    (9)

    (12): Reflective coating

    (9): B/S coating

    Beamsplitter/

    compensatorassembly (8)

    Primary mirror (3)

    Fold mirror

    (22)

    Lenses

    (23)

    0.525 m

    imager (28)

    1.02mimager (26)

    Dichroic

    (24)

    Solar

    input

    Compensator

    VIS/NIR-Quad Cell

    Dichroic

    Quad Cell

    (21)

    Lenses(20)

    Laser

    MetrologyDetection

    1.02 m

    filter (25)

    0.525 mfilter (27)

    Beam splitter

    Fold

    mirror

    (15) Laser Metrology Insertion

    MAESTRO

    Interface (2)

    PV InSb

    Detector

    Lens

    Lens Glare stop

    Dichroic

    1.55 m

    filter (19)

    I t ti t S/C B

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    Integration to S/C Bus

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    Solar Occultation

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    ACE Orbit

    650 km,74

    inclined

    circularorbit

    -90

    -60

    -30

    0

    30

    60

    90

    25-Jul 24-Aug 23-Sep 23-Oct 22-Nov 22-Dec 21-Jan 20-Feb 21-Mar 20-Apr 20-May 19-Jun 19-Jul

    La

    titude

    Day of Year

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    Timeline Jan. 1998 Proposal to CSA

    Feb. 2001 FTS and Imager CDR

    Mar. 2001 MAESTRO CDR

    Jun. 2001 Bus CDR Sept. 2002 S/C integration & test

    Mar. 2003 Instrument test (Toronto)

    May 2003 Final integration (DFL)

    Aug. 2003 Launch

    Sept. 2003 Commissioning

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    ACE TestingScience testing led by Kaley Walker and Mike Butler

    Integrate all instruments (FTS, MAESTRO and imagers)

    and characterize their performance in a simulated

    space environment

    Science Test Objectives:

    Determine performance of FTS using passive cooler

    Make gas cell measurements using FTS / MAESTRO

    Perform complete imager testing

    Characterize suntracker pointing coordinates

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    Instrument Calibration Facility (U of

    Toronto)

    Class 10000 clean-room with2.0 m diameter x 5.0 m Thermal Vacuum chamber

    ICF Control room

    TVAC window

    Cold Shroud

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    Testing the Passive Cooler

    Detectors cooled to ~ 89 K by

    directing the FTS passive cooler

    at the He target

    Multi-layer insulation (MLI)

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    Gas cell measurements

    to TVAC Window

    3000C Blackbody

    HgXe

    lampGas

    Cell

    Gas Cell

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    ACE-FTS Test Data & Results

    InSb bandMCT band

    Detector 89 K, Instrument Nominal Temperature, ~12.0 Torr N2O

    N2ON2O

    H2O

    H2O

    N2O

    CO2

    H2O

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    ACE-FTS InSb Spectra

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    400 420 440 460 480 500

    Wavelength [nm]

    -0.80

    -0.60

    -0.40

    -0.20

    0.00

    Absorp

    tionCellMeasurements[lo

    g(I/Io)]

    0.0

    2.0

    4.0

    6.0

    8.0

    10.0

    Smoothed

    NOAACross-sections[Units1E-19cm

    2]

    U. Toronto Gas Cell

    NO2 Absorption Spectrum

    Hi-resolution Data from NOAASmoothed with 1.6 nm FWHMTriangular Filter

    MAESTRO GasCell Data

    MAESTRO Response to NO2

    C.T. McElroy2003-04-03

    Pegasus XL Launch Vehicle

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    Pegasus XL Launch Vehicle

    Pegasus XL Close up

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    Pegasus XL Close-up

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    FTS-2 (PARIS) in Quebec

    W t l At h i

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    Waterloo Atmospheric

    Observatory Status of

    Observatory Site:

    Building completedAugust 2003.

    WAO

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    Conclusions ACE successfully launched Aug 12th, 2003.

    The satellite is currently undergoing

    commissioning.

    Initial science measurements to hopefullyoccur toward the end of October, 2003.

    Baseline duration of the mission is 2 years.