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The University of Toronto

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Title: The University of Toronto


1
The University of Torontos Balloon-Borne Fourier
Transform Spectrometer
  • Debra Wunch, James R. Drummond, Clive Midwinter,
    Kimberly Strong
  • University of Toronto
  • Hans Fast
  • Meteorological Service of Canada
  • Atmospheric Science from Space using Fourier
    Transform Spectrometry
  • 12th Workshop
  • Quebec City, May 18-20, 2005

2
Outline
  • Motivation
  • MANTRA high-altitude balloon campaign
  • FTS instruments on MANTRA
  • Instrument The University of Torontos FTS
  • History
  • Preparation for MANTRA
  • Results
  • Ground-based
  • Balloon-based
  • Conclusions and Future Work

3
Motivation MANTRA
  • Middle Atmosphere Nitrogen TRend Assessment
  • Investigates the changing chemical balance of the
    mid-latitude stratosphere, with a focus on the
    role of nitrogen chemistry on the depletion of
    ozone.
  • Scientific Objectives
  • Measurement of profiles of relevant chemical
    species
  • O3, NO, NO2, HNO3, HCl, ClONO2, N2O5, CFC-11,
    CFC-12, OH, H2O, N2O, CH4, J-values for O(1D) and
    NO2, aerosol, wind, pressure, temperature and
    humidity
  • Intercomparison between instruments using
    different measurement techniques
  • FTS, grating spectrometers, radiometers and
    sondes
  • Solar occultation, emission, in situ
  • Validation of satellite data
  • SCISAT ACE-FTS, MAESTRO
  • Odin OSIRIS, SMR
  • ENVISAT SCIAMACHY, MIPAS, GOMOS

4
Motivation MANTRA
  • High-altitude balloon platform
  • Float height around 40 km
  • He-filled balloon
  • Payload size around 2 m by 2 m by 2 m
  • Main gondola pointing system
  • Four campaigns 1998, 2000, 2002, 2004 in
    Vanscoy, Saskatchewan (52N, 107W)
  • Launch balloons during late summer stratospheric
    zonal wind turnaround
  • photochemical control regime
  • low winds allow for longer float times
  • launch window is August 26 September 5 at 52N

5
FTS Instruments on MANTRA
  • Measure most atmospheric trace gas species
    simultaneously
  • DU FTS on 1998, 2002, 2004
  • University of Denver
  • 30 years of flight heritage
  • 0.02 cm-1 resolution 700-1300 cm-1 spectral
    range
  • PARIS FTS on 2004
  • Portable Atmospheric Research Interferometric
    Spectrometer, U. of Waterloo
  • 0.02 cm-1 resolution 750-4100 cm-1 spectral
    range
  • An ACE FTS clone built in 2003/4 as a
    balloon-borne validation instrument
  • MSC FTS on 2002, 2004
  • Occultation mode instruments (solar absorption
    through sunrise/sunset)

6
The Role of the MSC FTS on MANTRA
  • Develop a Canadian capacity for balloon-borne FTS
    measurements
  • Compare a well-understood instrument (DU) with
    new Canadian instruments (MSC, PARIS)
  • Compare linear Michelson-type FTS with a
    pendulum-style FTS (PARIS)
  • Measure HCl, O3, N2O, CO2, CO, etc.
  • Complement MANTRAs science goals of measuring
    ozone depletion and the molecules that contribute
    to the ozone budget
  • Ground-based and balloon-based intercomparisons
  • Compare with ground-based instruments on-site and
    other balloon-borne instruments
  • Satellite validation

7
The MSC FTS History
  • Bomem DA2 instrument built in the 1980s
  • Purchased by the Meteorological Service of Canada
    (MSC)
  • Built as a ground-based instrument
  • Upgraded to a DA5 instrument with DA8 electronics
    (including the dynamic alignment) in the
    mid-1990s
  • Obtained by the University of Toronto from the
    MSC in 2001
  • 0.02 cm-1 resolution 1200-5000 cm-1 spectral
    range
  • InSb and MCT detectors that measure
    simultaneously, CaF2 beamsplitter
  • Flown on MANTRA 2002 and 2004
  • MANTRA 2002 flight was an engineering flight
  • Test of temperatures and voltages

8
The MSC FTS History
  • Original Software
  • Software contained user prompts in the form of
    pop-up boxes
  • Inaccessible housekeeping information
  • Control software embedded in hardware (bios)
  • Original Hardware and Electronics
  • Dependable dynamic alignment (compensation for
    motion in moving mirror)
  • Large electronics box with circa 1990s
    electronics boards and power supplies
  • Power consumption 140 W
  • Mass 90 kg

9
Tasks in Preparation for MANTRA 2004
  • Convert the MSC FTS from a ground-based FTS into
    an instrument that can take ground-based and
    balloon-based data
  • Update the software and electronics
  • Remove pop-up boxes
  • Use modern technology without compromising
    performance
  • Address issue of accurate pointing for solar
    occultation measurements

10
Preparation for MANTRA 2004
  • Re-engineered control of the dynamic alignment
    system
  • Almost entirely new electronics
  • 3 boards kept (DA), 7 discarded
  • Replaced two control computers with one low-power
    motherboard
  • Wrote control software in LabVIEW
  • Controls DA
  • Includes automated scheduler
  • No human intervention required
  • Full uplink and downlink capabilities
  • Housekeeping
  • Temperatures, voltages, interferograms
  • New power supply system
  • Vicor power supplies
  • New data acquisition system
  • USB 16-bit ADC for interferograms
  • USB 12-bit ADC for housekeeping

11
Preparation for MANTRA 2004 Results
  • Mass reduction
  • Electronics box no longer necessary
  • All necessary electronics fit into spectrometer
    box
  • Mass reduced from 90kg to 55kg
  • Power reduction
  • Power reduced from 140W to 65W due to new
    electronic components
  • Improves temperature performance less power
    means less heat
  • Now about half the mass/power of the other two
    FTS instruments

12
Preparation for MANTRA 2004 Pointing
  • Obtained a dedicated sunseeker that tracks the
    sun within 10 degrees in zenith and azimuth
  • Had flown before on other balloon campaigns
  • No longer dependent on main gondola pointing
    system
  • Only dependent on being pointed in general
    direction of sun
  • Would still get no data if payload rotated
    uncontrollably
  • True for any solar-mode instrument on payload

13
MANTRA 2004
  • Ground-based campaign
  • 5 dedicated ground-based instruments
  • Brewer, grating spectrometers
  • 43 days of measurements
  • Flight on September 1st at 834 am
  • Successful launch, followed by loss of commanding
    to the payload
  • Pointing system overheated before sunset
  • Payload began rotating
  • Two spectra recorded on each detector

14
MSC FTS Ground-Based Data
  • Good quality ground-based data
  • Can resolve CO, CO2, O3, CH4, N2O, HCl, H2O and
    other molecules
  • Data acquired during almost every clear-sky
    opportunity (10 days)
  • Can participate in the ground-based campaign
  • Can compute column amounts of O3, which every
    other ground-based instrument measures

15
MSC FTS Ground-Based Data
16
MSC FTS Flight Data
  • Two spectra (on each detector) during sunset on
    the first MANTRA 2004 flight at 91
  • acquired during rotation of payload at sunset
  • Signal-to-noise ratio reduced
  • lower SNR attributed to rotation of payload
    tracker at ends of its field of view
  • Resolution reduced
  • reduced resolution attributed to rotation of
    payload, temperature, poor alignment before
    flight?
  • Can resolve CO, CO2, O3, CH4, N2O, HCl, H2O
  • should be able to retrieve slant columns
  • No vertical profile retrievals possible

17
MSC FTS Flight Data
18
Conclusions and Future Work
  • New instrument is improvement over old
  • Lower power consumption
  • Lower mass
  • Robust software
  • Continued work
  • Build delta-tracker with larger field of view
  • Improve detector alignment system
  • Slant column amounts from balloon data
  • Intercomparisons of ground-based data
  • Future work
  • Fly FTS on MANTRA 2006 payload and get data from
    a full occultation

19
Acknowledgements
  • The authors wish to thank Pierre Fogal, John
    Olson, Tom McElroy, Kaley Walker and the MANTRA
    2002 and 2004 science teams.
  • Funding is provided by the Canadian Space Agency,
    the Meteorological Service of Canada and NSERC.
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