Minimize SciSat-1

SciSat-1/ACE (Science Satellite/Atmospheric Chemistry Experiment)

Spacecraft     Launch    Mission Status     Sensor Complement    Ground Segment    References

SciSat-1/ACE is a Canadian atmospheric science mission. In the time frame 1996/97, CSA (Canadian Space Agency) initiated the SciSat program with the objective to provide opportunities for Canadian scientists to define and conduct space experiments in the following fields: Earth sciences, space astronomy, and solar-terrestrial relations. Mission selection procedures in the program were conducted via an AO (Announcement of Opportunity) process and peer reviews. 1) 2) 3) 4) 5) 6) 7) 8) 9)

In addition, the SciSat program is also part of a CSA/NASA collaboration program, consisting of two missions. Under the terms of the cooperative agreement, each agency provides a spacecraft and instrumentation, to be co-launched on an expendable vehicle. The AO for the Canadian elements of the first SciSat (SciSat-1) was released in 1997. The ACE mission was selected for flight in November of 1998.

The SciSat/ACE mission is based at the University of Waterloo, Waterloo, Ontario (Mission Scientist: Peter Bernath). The overall objective is to monitor and analyze the chemical processes that control the distribution of ozone in the upper troposphere and stratosphere. In particular, ACE is focussing on one important and serious aspect of the atmospheric ozone problem - the decline of stratospheric ozone at northern mid-latitudes and in the Arctic. A comprehensive set of simultaneous measurements of trace gases, thin clouds, aerosols and temperature are being collected by solar occultation from low earth orbit. More than 30 molecules have been detected including: O3, N2O, CH4, HNO3, H2O, HCl, HF, NO, NO2, ClNO3, CO, CO2, CCl3F, CCl2F2, and N2O5.

SciSat_AutoB

Figure 1: Artist's view of the SciSat spacecraft (image credit: Bristol Aerospace)

Spacecraft:

The SciSat/ACE minisatellite structure, designed, built and integrated by Canadian industry (prime contractor: Bristol Aerospace Ltd. of Winnipeg, Manitoba, a division of Magellan Aerospace Corporation), uses a circular instrument/component aluminum mounting plate (1.12 m in diameter) as the main structure of the platform. The spacecraft is 3-axis stabilized. Attitude control is based on a bias momentum stabilization approach. The subsystem consists of a momentum wheel, torque rods (MTR-30 of SSTL) along all three body-fixed axes, one fine sun sensor, a magnetometer and a set of six coarse sun sensors. All sensors and actuators are off-the-shelf components with flight heritage. Pointing control provides ±1º in pitch and yaw axis (3σ) and ±2º in the roll axis (3σ). The CALTRAC™ star trackers were manufactured by CAL Corp, Canada (now COM DEV International). 10)

SciSat_AutoA

Figure 2: Artist's rendering of the SciSat spacecraft (image credit: Bristol Aerospace)

In addition, the GyroWheelTM (developed at Bristol AeroSpace) is flown for technology validation. The GyroWheel has the ability to provide the S/C simultaneously with stored angular momentum, to function as a 3-axis torque actuator, and to measure the S/C angular rates in two axes. The GyroWheel is a CMG (Control Moment Gyroscope) device and as such an actuator/sensor demonstration experiment. The design is based on a spinning flex-gimbal system as opposed to the conventional non-spinning motor-driven gimbals. This innovation allows for maintaining the same three-axis momentum steering capability as a CMG. The primary benefit of the CMG design that it allows for substantial savings in mass (eliminating the need for multiple momentum wheels and gyros), power, and cost of the attitude control system. - Flight testing of GyroWheel was carried out mainly during periods when science is not being conducted. After its validation, the GyroWheel is expected to operate as the primary wheel and will used during science operations. The performance of the GyroWheel is now validated and it functions as a back-up system. The GyroWheel is functionally redundant with the momentum wheel. 11) 12)

Parameter

Value

Parameter

Value

Instrument mass

5.9 kg @ 4 Nms torque
7.4 kg @ 16 Nms

Instrument power

15.7 W @ 1500 rpm
101 W @ 6000 rpm

Min reaction torque
- Spin axis
- Tilt axis


76 mNm (at 1200 rpm)
122 mNm (at 0º tilt)

Command & data I/F

Design life

Serial RS-422, or
MIL-STD-155B
≥ 10 years

Gyro bias stability

≤ 1º/ hr

Speed range

1200-6000 rpm

Max rotor tilt angle

±7º

Onboard processing

16 MIPS total

Radiation tolerance

100 krad (Si) total dose

Input voltage

28±6 V

Instrument size

23.5 cm dia x 13.5 cm

Static balance

≤ 1 gm-cm

Table 1: Characteristics of the GyroWheel

SciSat_Auto9

Figure 3: Illustration of the GyroWheel (image credit: Bristol AeroSpace)

The spacecraft is always in a sun-pointing configuration. S/C power (75 W orbital average, triple junction solar cells, GaIn/GaIn/Ge, one of them is a Si cell) is generated by a single body-mounted solar panel. In addition, there are Lithium-Ion batteries (13.6 Ah capacity) for the orbital eclipse phase operations.

On-board source data recording of up to 1.5 GByte is provided. The C&DH (Command & Data Handling) unit was developed for small satellites. It is responsible for all onboard data handling, monitoring and recording. The unit features low-power (≤ 10 W), low-mass (≤ 4 kg) and a radiation-tolerant core in a single string architecture (a UTMC 80C196 16-bit processor is used to perform all S/C operations). The instruments are connected to C&DH via a synchronous RS-422 interface. The S/C mass is 152 kg (payload mass = 47 kg), the design life is two years with a goal of five years. 13)

SciSat_Auto8

Figure 4: 2. The scientific instruments and some of the bus components aboard SciSat-1 (image credit: Bristol Aerospace)

 

Launch: A NASA-sponsored launch of SciSat/ACE took place on Aug. 13, 2003 (UTC) on a Pegasus-XL vehicle (air launch) from VAFB (Vandenberg Air Force Base), CA.

RF communications are provided in S-band using the CCSDS protocol suite. Variable-rate telemetry downlinks can be supported (4, 2, 1, 0.5 , or 0.04 Mbit/s). The downlink uses OQPSK (Offset Quadrature Phase Shift Keying) modulation, and the uplink is compatible with NASA's STDN (Satellite Tracking and Data Network) standards. The maximum data rate (occurring during an occultation) is about 9.6 Mbit/s, and almost all of it come from the ACE-FTS instrument. The uplink data rate is 4 kbit/s. Reed Solomon (RS) encoding is used on the downlink to achieve a 1 x 10-9 bit error rate. Spacecraft tracking and orbit determination is done using coherent Doppler tracking. The ACE-FTS raw data volume is about 2 GByte/day.

Orbit: Circular high-inclination orbit, altitude = 650 km, inclination = 73.9º, period = 97.7 minutes. No onboard propulsion is available for orbit maintenance. The ACE orbit was selected so that the latitude coverage repeats annually (Figure 5).

SciSat_Auto7

Figure 5: Latitude coverage of the ACE-FTS for one year (image credit: University of Waterloo)

SciSat_Auto6

Figure 6: Illustration of the SciSat-1 spacecraft and payload, three views (image credit: ABB Bomem)

 


 

Mission status:

• In January 2017, the SciSat mission continues to operate nominally according to Peter F. Bernath, who heads the SciSat science team. The project at the University of Waterloo has a contract with CSA (Canadian Space Agency) until 2018 (but this will very likely be extended). The SciSat mission provides data to academia, space agencies, governmental and scientific organizations around the world. 14)

- The ACE (Atmospheric Chemistry Experiment) on SciSat measures chemical molecules that influence the distribution of stratospheric ozone, particularly in the Arctic. These data are making an important contribution to international environmental policy making aimed at protecting the ozone layer, such as the Montreal Protocol that bans certain CFCs. ACE measures the absorption of solar light by the atmosphere at sunrise and sunset. Different atmospheric constituents absorb different wavelengths of light in characteristic ways—a signature by which they can be identified. This technique is what allows ACE to make extremely accurate measurements. 15)

- With its instrument performing so well, SCISAT is now moving beyond its original mandate and providing excellent data related not only to ozone depletion, but also to climate change, and air quality and pollution. "There are many things we're doing now that we really didn't know we could do," Bernath said.

- ACE observations are also useful in climate studies. For example, they've shown that previously observed increases in the amount of water vapor being injected into the stratosphere have stopped. Water vapor is the most powerful natural greenhouse gas and plays a key role in the Earth's climate. "No one knew why it was increasing and we don't know why it stopped, so there are quite a few mysteries left," said Bernath.

• In October 2015, Canada's SciSat mission is 12 years on orbit with its 2 instruments, ACE-FTS and MAESTRO. The high-resolution ACE-FTS (Atmospheric Chemistry Experiment -Fourier Transform Spectrometer) is operating in the solar occultation mode in Earth-orbit. ACE-FTS retrieves vertical profiles of temperature, pressure, and volume mixing ratio of 38 molecular species, and relies on international cooperation to validate its data products. Data availability from international Earth-observing missions is vital to interpreting domestic results, and ACE-FTS validation uses data products from 12 instruments and 7 space agencies. 16)

- The data of the Taiwan/US FormoSat-3/COSMIC constellation mission are being used and incorporated into the ACE-FTS data validation campaign. The FormoSat-3/COSMIC mission of six small satellites uses signals from GPS satellites to measure water vapor pressure and temperature via radio occultation. These data are compared to those retrieved by the ACE-FTS instrument on SciSat along with a newly developed algorithm applied to ACE-FTS spectra. The new algorithm to retrieve vertical profiles of temperature and pressure from high-resolution solar transmission spectra was developed in support of a partnership between the CSA and NASA/JPL (Jet Propulsion Laboratory) to place an FTS in orbit around Mars as part of the ESA and NASA's joint ExoMars mission (NASA since withdrew). — This algorithm exploits the temperature dependence of individual absorption lines in an infrared vibration-rotation band. ACE-FTS makes multiple measurements during an occultation, separated by 1.5-5 km, and the project analyzes 10 CO2 vibration-rotation bands at each altitude, each with a different usable altitude range. The retrieved profiles have no seasonal or zonal biases, but do have a warm bias in the stratosphere and a cold bias in the mesosphere, with mean differences less than 5 K when compared to ACE-FTS. The FormoSat-3/COSMIC comparisons are done below 40 km where the best agreement prevails with FTS-ACE data and the mean differences are less than 3 K. The H2O comparisons between ACE-FTS and FormoSat-3/COSMIC show good agreement in the stratosphere, and higher concentrations retrieved by COSMIC in the troposphere.

- Over its lifetime of 12 years in orbit, ACE-FTS has been well validated by satellite, ground-based, and balloon-borne instruments to establish the accuracy and reliability of the ACE-FTS data products. Published temperature validation results used three satellite instruments, nine ground-based instruments, one balloon instrument and sondes launched from several sites. The satellite instruments were: SABER (Sounding of the Atmosphere using Broadband Emission Radiometry) instrument on the TIMED (Thermosphere Ionosphere Mesosphere Energetics and Dynamics) spacecraft, MIPAS (Michelson Interferometer for Passive Atmospheric Sounding) on Envisat, and the HALOE (Halogen Occultation Experiment) on UARS (Upper Atmosphere Research Satellite). TIMED and HALOE are NASA instruments, while MIPAS was developed by ESA (European Space Agency).

SciSat_Auto5

Figure 7: Initial ACE-FTS water vapor validation results incorporating the COSMIC 2013 reanalysis data product. (image credit: University of Toronto, University of Waterloo, NASA/JPL)

Legend to Figure 7: Shown are: number of coincidences, correlation coefficient, mean relative differences, and the standard deviation of the mean relative differences. Instruments used in the validation are: HALOE, MAESTRO, MIPAS, MLS, POAM III, SAGE III, SMR, and COSMIC. MIPAS has data products from two retrieval software versions by ESA and IMK (Institute of Meteorology and Climate Research), formerly the Karlsruhe Research Center, Karlsruhe, Germany.

• Nov. 6, 2014: Thanks to Canada's SciSat mission, an international team of scientists has discovered a recent and unexpected increase in stratospheric hydrogen chloride (HCl) in the Northern Hemisphere. 17) 18)

- Information from SciSat along with other satellite data and ground-based measurements showed the scientific team that the increase in stratospheric HCl is due to a slowdown in the atmospheric circulation of the Northern Hemisphere. This discovery could impact how scientists will analyze the evolution of the stratospheric ozone layer going forward.

- Since 1989, the implementation of the UN's Montreal Protocol has led to a reduction in chlorofluorocarbons (CFCs) around the globe. These CFCs are responsible for the depletion of the ozone layer that protects us from ultraviolet radiation. CFCs break-up in the stratosphere and release chlorine atoms that then form HCl. Under certain conditions, HCl can be transformed into other chlorine-containing molecules that destroy ozone.

- The SciSat data was essential in identifying the altitudes at which this change was taking place. Without reliable HCl measurements in the lower stratosphere provided by the Canadian instrument, we could not have reached this conclusion. No other single instrument has provided such a wide range of data products for such a long time.

• Oct. 2014: SciSat has been operating more than 5 times its design lifetime. The mission has been highly successful and its scientific return far exceeded initial hopes. Starting from a dedicated ozone characterization experiment, the SciSat data are now used worldwide to monitor many chemical species in the atmosphere impossible to observe with any other instruments. Hence, there is a strong interest and value in assuring the continuity of the measurements made with SciSat. 19)

- The ACE-FTS was designed for a 2-year mission. The parts selection & qualification level, the redundancy scheme, the shielding, the life testing of critical elements have all been done with a 2-year mindset and a scientific mission risk profile. After more than 11 years on orbit, the SNR performance still exceeds the original requirement (100) by a factor of up to 4x in certain spectral regions. No anomaly was observed to date despite the fact that early during its mission life, the SciSat-1 spacecraft had to face a violent and severe solar storm. SciSat remains the only sensor in orbit providing long term trending of low concentration molecules within the atmosphere. This is a key contribution to the assessment of climate change.

- Various studies have been conducted for potential SciSat follow-on. One of these missions is the CASS (Chemical and Aerosol Sounding Satellite) mission. The goals of the CASS mission are to further expand our understanding of:

1) How the Earth's atmospheric composition is evolving and responding to both natural and anthropogenic changes.

2) The coupling between the recovery of the ozone layer from the effect of ozone-depleting substances and climate change.

3) The processes and dynamics that control the role of the upper troposphere/lower stratosphere (UT/LS) region and the links with the surface climate.

CASS also has for objectives to fill a potential data gap between the current limb sounding mission and the future limb sounding missions. To achieve these goals, CASS is planned to carry an improved version of the ACE-FTS with enhanced capabilities.

The Phase 0 of CASS was completed in Spring 2012 and experimental demonstration of critical subsystem was completed in the summer of 2014. - The CSA (Canadian Space Agency) has also been considering many other missions involving FTS technology in the past years. None of these missions are currently funded but preliminary studies have been conducted for them and discussions for international collaboration have been taking place (Ref. 19).

• January 2014: The SciSat/ACE spacecraft and its payload continue to operate nominally. The current extension of the mission is to July 2014. However, ACE is currently undergoing a major review, and a further extension of the mission may be the outcome (Ref. 22).

• In August 2013, the SciSat/ACE spacecraft was completing 10 years on orbit. The project team and CSA are proud of the unique measurement capabilities of this small Canadian satellite and of the large role that this space mission plays in monitoring stratospheric ozone and its associated chemistry. SciSat helps a team of Canadian and international scientists improve their understanding of the depletion of the ozone layer, with a special emphasis on the changes occurring over Canada and in the Arctic. 20)

- SciSat has surpassed expectations by lasting 10 years to date. It delivers valuable data on climate change, air quality and pollution in support of international environmental policy aimed at protecting the ozone layer. The tenth anniversary of the first science data downloaded from SCISAT will be marked by a scientific workshop held at York University in Toronto from October 23 to 25, 2013.

- Originally planned as a two-year mission, SciSat's instruments continue to provide information about more than 30 different molecular species, which is more than have ever been thoroughly measured from space. SciSat delivers excellent data related not only to ozone depletion, but also to climate change, air quality and pollution. Undoubtedly, SciSat's mission is a great Canadian success story.

- On October 22, 2013 at the University of Toronto, scientists, government representatives and industry partners participated in a media event to celebrate a decade of success for Canada's SciSat/ACE satellite mission. The tenth anniversary of the first science data observations from SciSat/ACE will also be marked by a scientific workshop at York University in Toronto from October 23-25, 2013. 21)

• In April 2013, the SciSat/ACE spacecraft and its payload are operating nominally. 22)

• On August 13, 2012, the SCISAT/ACE project marked the 9th anniversary of the mission in orbit (2 year design life). Since launch, the satellite and instrument operations are nominal. 23)

- On 8 June 2012, SCISAT completed its 47,500th orbit!

- Profiles available for ~29,000 occultations

- ~50% of occultations occur in polar regions (> 60 degrees)

- Operation of ACE mission approved until the end of March 2014.

• In 2012, the SCISAT/ACE instruments and satellite are continuing to function nominally and produce excellent results (deriving altitude profiles of over 30 different atmospheric trace-gas species, temperature and pressure) after more than 8 years on orbit (Ref. 25). 24)

• The SciSat-1 spacecraft and its payload are operating nominally in 2011. 25)

• In the early part of 2010 (February 20 -April 1), the "Canadian ACE Arctic Validation Campaign" was conducted with a suite of ground-based instruments which were deployed making measurements of trace gases to assess the measurements of ACE-FTS on SciSat. The campaign took place at the PEARL (Polar Environment Atmospheric Research Laboratory) facility located in Eureka, Nunavut (Canada).

• The SciSat-1 spacecraft and its payload are operating nominally in 2010 (in its 7th year of operations, 2 years of nominal design life). CSA intends to keep the very successful mission operating. 26) 27) 28)

• In 2009 the spacecraft is operating nominally, there is no degradation in performance of the FTS or of the satellite bus. The only issue is for the wavelength limits of the MAESTRO instrument: they are now decreased to 450-1000 nm. Fortunately this does not have much impact on the primary MAESTRO science (NO2 and O3 profiles plus atmospheric extinction). - CSA has committed to supporting the mission at least until March 31, 2010.

• SciSat provides high-precision information on the condition of the ozone layer and atmospheric changes. In 2006, data collected by SciSat played a key role in helping scientists better understand the loss of ozone over the Northern hemisphere.

• As of mid-April 2006, the ACE satellite instruments had made more than 10,000 occultation measurements. No degradation of ACE-FTS instrument performance or functionality was observed since launch. 29) 30) 31) 32) 33)

• In August 2005, SciSat-1 met its mission life requirements of 2 years. CSA decided to extend the funding for SciSat-1/ACE mission operations (mission life) for two more years.

• After 6 months of commissioning and test phase the spacecraft was declared fully operational on February 27, 2004 (start of science mission). 34)

• On October 22, 2003, the first data observations from SciSat/ACE were acquired.

 


 

Sensor complement: (ACE-FTS, MAESTRO)

ACE-FTS (Atmospheric Chemistry Experiment-Fourier Transform Spectrometer)

ACE-FTS is the prime instrument of the SciSat mission. ACE has been built by ABB Bomem Inc. of Quebec City, Quebec. The objective is to measure the vertical distribution of atmospheric trace gases, in particular of the regional polar O3 budget, as well as pressure and temperature (derived from CO2 lines). The instrument is an adapted version of the classical sweeping Michelson interferometer, using an optimized optical layout (Figure 10).

ACE consists of the following components: the FTS, a VNIR (Visible Near Infrared) imager, a sun tracker, the instrument electronics, and a power supply. An SNR > 100 is achieved; IFOV (FTS) = 1.25 mrad; a telescope aperture diameter of 100 mm and a measurement period of 2 s. The instrument includes a suntracker, which provides fine pointing toward the radiometric center of the sun with a stability better than 15 µrad, to both the infrared spectrometer and the imager during solar occultation of the Earth's atmosphere (there are about 30 sun occultation periods per day). Measurements can be made in the altitude range 5-150 km. The FTS is coupled with an auxiliary 2-channel VNIR imager. 35) 36) 37) 38) 39) 40) 41)

The operation of the ACE-FTS in solar occultation provides a reproducible evaluation of the temperature profile. In fact, since the radiance of the sun is used as the radiometric reference for the instrument, the temperature sounding is much less sensitive to manufacturing variability from one unit to the other or to the ageing of the hardware. This is a key advantage for global climatology where trends over decades must be accurately measured.

• The FTS spectrometer looks at the sun through the atmosphere (occultation or limb-viewing geometry) at different tangent heights, providing a series of spectra that are used to deduce the vertical distribution of trace gases and temperature. The spectral range of the instrument is from 2-13 µm (750 - 4100 cm-1) in two bands, and the maximum resolution is 0.025 cm-1. InSb (1800-4100 cm-1) and HgCdTe (750-1800 cm-1) detectors are used. Both detectors are cooled below 110 K. The spectrometer transforms the spectra into a modulated signal, the interferogram, in which all of the IR bands are present simultaneously. The spectrometer output consists of such interferograms for each observed scene. The interferograms are Fourier-transformed into spectra on the ground to provide vertical profiles of atmospheric constituents at vertical resolutions of 3-4 km.

VNIRI (Visible Near Infrared Imager). Objective: monitoring of aerosols using the method of extinction of solar radiation. Two filtered detectors at 1.02 and 0.525 µm are employed. VNIRI provides sun images in two spectral bands at 0.525 µm and at 1.02 µm. Refractive index distortion of the solar image for low altitude measurements is monitored with a large CMOS photodetector array of 128 x 128 effective elements covering 30 mrad with a pixel separation of 0.25 mrad (the IFOV is more than four times smaller than the IFOV of the FTS). These measurements have an SNR>100 for all sun-illuminated pixels in a two-second observation time. The sun tracker keeps the instruments (FTS and VNIRI) automatically pointed at the sun's radiometric center.

Parameter

Value

Parameter

Value

Spectral range

2.4-13.3 µm
(or 750-4100 cm-1)

Noise equivalent radiance

<0.5% of the radiance of a blackbody at 5800 K

Spectral resolution cm-1

<0.028, 0.056, 0.11, 0.55

Detectors

InSb, HgCdTe

Sweep duration

2, 1, 0.5, 0.1 s

Detector cooling

Passive cooling <100 K

Spectral stability (relative)

3 x 10-7 rms for 180 s

FOV (Field of View)

1.25 mrad

Table 2: Characteristics of the ACE-FTS instrument

SciSat_Auto4

Figure 8: The FTS interferometer (image credit: ABB Bomem)

SciSat_Auto3

Figure 9: Illustration of the optics side of the ACE-FTS instrument, front cover removed (image credit: ABB Bomem)

The main design drivers of the ACE-FTS instrument are sensitivity (SNR), spectral resolution and large spectral coverage. The spectrometer is an adapted version of the classical Michelson interferometer using an optimized optical layout. The instrument optics are based on a highly folded design and results in a very compact high performance instrument as shown in Figure 10. The first optical component is the suntracker module that tracks the radiometric center of the sun. The infrared and visible signals are then directed to a 5X magnification telescope primary mirror. A small bandpass filter, mounted on the primary telescope mirror, transmits the 1.52 µm to 1.59 µm spectral range to a quad cell (used as the feedback source for the suntracker module) and reflects the remaining spectrum to the VIS/NIR imager. The primary mirror reflects the signals through the aperture and field stops to the secondary collimation mirror. Then, the collimated beam is directed towards the interferometer. A filter is installed between the input optics and the interferometer to minimize the thermal load on the interferometer. The output of the interferometer is then condensed to the InSb/MCT detector assembly using an off-axis parabola. The ACE-FTS instrument has a mass of about 35 kg, power 40 W operating, and 15 W in standby.

Note: The ACE-FTS mission based on ATMOS (Atmospheric Trace Molecule Spectrometer), a JPL instrument which flew four times on the Space Shuttle (1985, 1992, 1993, and 1994). However, the ACE-FTS instrument has been miniaturized by nearly a factor of 10 in terms of mass, power and volume as compared to ATMOS.

SciSat_Auto2

Figure 10: Optical layout of the ACE-FTS instrument (image credit: ABB BOMEM)

 

MAESTRO (Measurement of Aerosol Extinction in the Stratosphere and Troposphere Retrieved by Occultation)

MAESTRO was designed and built in a partnership between MSC (Meteorological Service of Canada), EMS Technologies of Ottawa, and the University of Toronto. The design of MAESTRO is of CPFM (Composition and Photodissociative Flux) heritage, an airborne instrument developed at the Meteorological Service of Canada, which has flown on numerous ER-2 aircraft missions. 42) 43)

MAESTRO is a dual-channel optical spectrometer in the spectral region of 285-1030 nm. The objective is to measure ozone, nitrogen dioxide and aerosol/cloud extinction (solar occultation measurements of atmospheric attenuation during satellite sunrise and sunset with the primary objective of assessing the stratospheric ozone budget). Solar occultation spectra are being used for retrieving vertical profiles of temperature and pressure, aerosols, and trace gases (O3, NO2, H2O) involved in middle atmosphere ozone distribution. - The use of two overlapping spectrometers (280 - 550 nm, 500 - 1030 nm) improves the stray-light performance. The spectral resolution is about 1-2 nm.

SciSat_Auto1

Figure 11: Illustration of the MAESTRO instrument (image credit: MSC)

The detectors are linear EG&G Reticon photodiode arrays with 1024 elements. The instrument design is based on a simple concave grating with no moving parts. The entrance slit is held horizontal to the horizon during sunrise and sunset by controlling the spacecraft roll with a startracker and a momentum wheel on the satellite bus. The vertical resolution of the MAESTRO data is about 1 km; the SNR is >1000. The high vertical resolution may help to distinguish between various atmospheric layers. The oxygen A-band at 762 nm (as well as the B-band and gamma-band) will be used to make an independent determination of atmospheric temperature and pressure. MAESTRO is also able to make some near-nadir solar backscatter measurements with a separate backscatter port. The mass of the instrument is about 8 kg, power = 15 W (operating), 7 W (standby), the data rate = 3 Mbit/s.

SciSat_Auto0

Figure 12: Schematic of the MAESTRO instrument (image credit: MSC)

The measurements obtained by the ACE-FTS and MAESTRO instruments are being combined with data gathered by ground-based, balloon-based and other space-based projects to obtain the best possible information to predict future trends relating to the ozone layer and its depletion.

 


 

Ground segment:

The SciSat ground segment consists of a SOC (Science Operations Centre), based at the University of Waterloo, and a MOC (Mission Operations Centre) at CSA in Saint-Hubert (along with a ground station), Quebec, and a second ground station in Saskatoon, Saskatchewan. In addition, there is an ESA ground station at Kiruna, Sweden, and a NASA ground station at Fairbanks, AK.

At the SOC the data is archived and transformed into data products for distribution to the science team members. The data analysis of SciSat is based on the cooperation of many national and international partners. The science team includes researchers from Canada, USA, Belgium, Japan, France, and Sweden.

Raw data is transformed first into reflectance spectra as function of altitude (Level 1) and then into vertical profiles of concentration for various atmospheric constituents (Level 2). Data processing is conducted by the ACE Science Team based at the University of Waterloo. The following paragraph gives a list of the molecules retrieved routinely by the ACE-FTS Level 2 processing (version 3.0): 44)

H2O, O3, N2O, CO, CH4, NO, NO2, HNO3, HF, HCl, N2O5, ClONO2, CFC-12 (CCl2F2), CFC-11 (CCl3F), COF2, HCFC-22 (CHClF2), HDO, SF6, OCS, HCN, CF4, CH3Cl, C2H2, C2H6, N2, CO2, H2CO, H2O2, O2, HO2NO2, HCOOH, CH3OH, COCl2, CCl4, COClF, HCFC-142b (ClF2C-CH3), CFC-113 (Cl2FC-CClF2), HCFC-141b (Cl2FC-CH3), as well as isotopologues for some of these molecules.

 


1) "ACE: Atmospheric Chemistry Experiment," URL: http://www.ace.uwaterloo.ca/

2) P. F. Bernath, C. T. McElroy, M. C. Abrams, C. D. Boone, M. Butler, C. Camy-Peyret, M. Carleer, C. Clerbaux, P.-F. Coheur, R. Colin, P. DeCola, M. DeMaziere, J. R. Drummond, D. Dufour, W. F. J. Evans, H. Fast, D. Fussen, K. Gilbert, D. E. Jennings, E. J. Llewellyn, R. P. Lowe, E. Mahieu, J. C. McConnell, M. McHugh, S. D. McLeod, R. Michaud, C. Midwinter, R. Nassar, F. Nichitiu, C. Nowlan, C. P. Rinsland, Y. J. Rochon, N. Rowlands, K. Semeniuk, P. Simon, R. Skelton, J. J. Sloan, M.-A. Soucy, K. Strong, P. Tremblay, D. Turnbull, K. A. Walker, I. Walkty, D. A. Wardle, V. Wehrle, R. Zander, J. Zou, "Atmospheric Chemistry Experiment (ACE): Mission overview," Geophysical Research Letters, Vol. 32, L15S01, doi:10.1029/2005GL022386, 2005, URL: http://earth.esa.int/pub/ESA_DOC/SCISAT/3RDPARTY42.pdf

3) P. Bernath, "Atmospheric Chemistry Experiment: Spectroscopy from Orbit," Optics & Photonics News, Optical Society of America, April 2005, pp. 24-27.

4) H. Dahl, W. Eliuk, G. Rumbold, R. Shelly, "ACE - A Canadian Small Satellite Mission," Proceedings of the 13th AIAA/USU Conference on Small Satellites, Aug. 23-26, 1999, Logan UT, SSC99-V-7, URL: http://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=2151&context=smallsat

5) I. Walkty, J. Petersen. T. Doherty, B. Whitehead, "SCISAT-1 ACE Mission C&DH Unit Development," Proceedings of the 14th Annual AIAA/USU Conference on Small Satellites, Logan, UT, Aug. 21-24, 2000, SSC00-I-5

6) P. Bernath, "The Atmospheric Chemistry Experiment (ACE): An Overview," Proceedings of IGARSS 2002, Toronto, Canada, June 24-28, 2002

7) Chris Boone, Peter Bernath, "SciSat-1 mission overview and status," Proceedings of SPIE, Vol. 5151, 'Earth Observing Systems VIII,' edited by William L. Barnes, 2003, URL: http://www.ace.uwaterloo.ca/publications/2003/BooneSPIEinvitedPaper.pdf

8) P. Bernath, "Atmospheric Chemistry Experiment (ACE): An Overview," Spectroscopy from Space, J.Demaison, editor, Kluver, 2001

9) P. F. Bernath, " Atmospheric Chemistry Experiment (ACE): Analytical Chemistry from Orbit," Trends in Analytical Chemistry, Vol. 25, No. 7., 2006, pp. 647-654, URL: http://www.ace.uwaterloo.ca/publications/BernathACE-AnalyticalRev2006reprint.pdf

10) A. Denis, S. Page, I. Walkty, "The Evolution of a SciSat-1 Spacecraft to Provide a Generic Small Satellite Bus for the Canadian Space Agency," Proceedings of IAC 2004, Vancouver, Canada, Oct. 4-8, 2004, IAC-04-IAA.4.11.2

11) M. Senez, N. Pokrupa, B. Taylor, D. Staley, M. Vinnins, " The GyroWheelTM Testing and Flight Qualification Program," AAS Guidance and Control Conference 2002, Breckenridge, CO, Feb. 6-10, 2002

12) G. Tyc, D. A. Staley, W. R. Whitehead, et al., "GyroWheelTM - An Innovative new Actuator/Sensor for Spacecraft Attitude Control," 13th AIAA/USU Conference for Small Satellites, Aug. 23-26, 1999, Logan UT, SSC99-XI-8

13) I. Walkty, J. Petersen, T. Doherty, B. Whitehead, "SciSat-1 ACE Mission C&DH Unit Development," Proceedings of the AIAA/USU Conference on Small Satellites, Logan, UT, 2000, SSC00-I-5

14) Information provided on January 17, 2017 by Prof. Peter F. Bernath, Old Dominion University, Norfolk, VA, USA.

15) "SCISAT/ACE: an important asset for international environmental policy," CSA, Dec. 9, 2016, URL: http://www.asc-csa.gc.ca/eng/satellites/scisat/

16) Kevin S. Olsen, Geoff C. Toon, Chris D. Boone, Patrick E. Sheese, Kaley A. Walker, Kimberly Strong, "Intercomparison of water vapour and temperature retrievals between the CSA's ACE-FTS and the UCAR/NSPO's COSMIC/Formosat-3 satellites, and presentation of a new algorithm for retrieving temperature," Proceedings of the 66th International Astronautical Congress (IAC 2015), Jerusalem, Israel, Oct.12-16, 2015, paper: IAC-15-B1.1.7

17) "Canada's SCISAT Satellite makes important discovery for understanding the evolution of the ozone layer," Government of Canada, Nov. 6, 2014, URL: http://news.gc.ca/web/article-en.do?nid=901089

18) E. Mahieu, M. P. Chipperfield, J. Notholt, T. Reddmann, J. Anderson, P. F. Bernath, T. Blumenstock, M. T. Coffey, S. S. Dhomse, W. Feng, B. Franco, L. Froidevaux, D. W. T. Griffith, J. W. Hannigan, F. Hase, R. Hossaini, N. B. Jones,I. Morino, I. Murata, H. Nakajima, M. Palm, C. Paton-Walsh, J. M. Russell III, M. Schneider, C. Servais, et al., "Recent Northern Hemisphere stratospheric HCl increase due to atmospheric circulation changes," Nature, Vol. 515, pp: 104–107, 06 November 2014, doi:10.1038/nature13857

19) Louis Moreau, Frederic Grandmont, Henry Buijs, Marc-Andre Soucy, "A decade of Fourier-Transform Spectrometers in space: overview of a Canadian signature technology," Proceedings of the 65th International Astronautical Congress (IAC 2014), Toronto, Canada, Sept. 29-Oct. 3, 2014, paper: IAC-14-B1.3.3

20) "SciSat - 10 years of success," August 12, 2013, URL:
http://www.asc-csa.gc.ca/eng/satellites/scisat/default.asp

21) "Canadian Satellite SCISAT Celebrating 10 Years of Scientific Measurements," Digital Journal, Oct. 22, 2013, URL: http://www.digitaljournal.com/pr/1539754

22) Information provided by Peter Bernath of the Old Dominion University, Norfolk, VA, USA.

23) Kaley A. Walker, Peter Bernath, C. Thomas McElroy, "Solar Occultation Measurements of Atmospheric Composition: SCISAT/ACE and beyond," Proceedings of ATMOS 2012, Advances in Atmospheric Science and Applications, Bruges, Belgium, June 18-22, 2012, URL: http://congrexprojects.com/docs/12m06_docs2/2_walker_esa-atmos2012-18jun2012.pdf

24) Kaley A. Walker, C. Thomas McElroy, Peter F. Bernath, "Composition Measurements by Solar Occultation: SciSat/ACE and beyond," Proceedings of the 2011 EUMETSAT Meteorological Satellite Conference, 5-9 September 2011, Oslo, Norway, URL: http://www.eumetsat.int/Home/Main/AboutEUMETSAT/Publications
/ConferenceandWorkshopProceedings/2011/groups/cps
/documents/document/pdf_conf_p59_s1_14_walker_v.pdf

25) Information provided by Peter Bernath of the University of Waterloo, Waterloo, Ontario, Canada

26) Information provided by Peter F. Bernath of York University

27) S. R. Beagley, C. D. Boone, V. I. Fomichev, J. J. Jin, K. Semeniuk, J. C. McConnell, P. F. Bernath, "First multi-year occultation observations of CO2 in the MLT by ACE satellite: observations and analysis using the extended CMAM," Atmospheric Chemistry and Physics, Vol. 10, 2010, pp.1133-1153, URL: http://www.atmos-chem-phys.org/10/1133/2010/acp-10-1133-2010.pdf

28) Frank Hase, Lloyd Wallace, Sean D.McLeod, JeremyJ.Harrison, Peter F. Bernath, "The ACE-FTS atlas of the infrared solar spectrum," Journal of Quantitative Spectroscopy& Radiative Transfer, Vol. 111, 2010, pp. 521–528

29) P. F. Bernath, "Atmospheric Chemistry Experiment (ACE): Mission Status," Proceedings of the Atmospheric Science Conference 2006, ESA/ESRIN, Frascati, Italy, May 8-12, 2006

30) K. A. Walker, C. Boone, R. Skelton, S. D. McLeod, P. F. Bernath, C. E. Randall, C. R. Trepte, K. Strong, C. T. McElroy, "Recent Validation Results for the Atmospheric Chemistry Experiment (ACE)," Proceedings of the Atmospheric Science Conference 2006, ESA/ESRIN, Frascati, Italy, May 8-12, 2006

31) F. Châteauneuf, M.-A. Soucy, S. Fortin, "ACE-FTS instrument: after two years on-orbit," SPIE Conference on Optics & Photonics 2005, Vol. 5883, San Diego, CA, July 31-Aug. 4, 2005

32) "Canada's SCISAT Satellite in Full Operation," URL:
http://www.spaceref.com/news/viewpr.html?pid=13831

33) D. Kotelko, Ian Walkty, W. Czyrnyj, S. McLeod, "SCISAT-1 Mission Experience," Proceedings of the 13th Canadian Astronautics Conference, ASTRO 2006, Montreal, QC, Canada, organized by CASI (Canadian Astronautics and Space Institute), April 25-27, 2006

34) SCISAT Mission status update," CSA, Feb. 2004

35) M.-A. Soucy, F Châteauneuf, R. Skelton, S Fortin, "ACE-FTS Instrument:: After two and a half years in orbit," Proceedings of the 13th Canadian Astronautics Conference, ASTRO 2006, Montreal, QC, Canada, organized by CASI (Canadian Astronautics and Space Institute), April 25-27, 2006

36) P. F. Bernath, "Atmospheric Infrared Fourier Transform Spectroscopy from Orbit," Proceedings of the 13th Canadian Astronautics Conference, ASTRO 2006, Montreal, QC, Canada, organized by CASI (Canadian Astronautics and Space Institute), April 25-27, 2006

37) M.-A. Soucy, C. Deutsch, F. Châteauneuf, "Status of the ACE-FTS Instrument," Proceedings of IGARSS 2002, Toronto, Canada, June 24-28, 2002

38) P. Bernath, "Atmospheric Chemistry Experiment (ACE): An Overview," Proceedings of SPIE, Vol 4814, SPIE Annual Meeting 2002: Remote Sensing and Space Technology, July 7-11, 2002, Seattle, WA

39) M.-A. Soucy, F. Chateauneuf, C. Deutsch, N. Etienne, "ACE-FTS Instrument Detailed Design," Proceedings of SPIE, Vol 4814, SPIE Annual Meeting 2002: Remote Sensing and Space Technology, July 7-11, 2002, Seattle, WA

40) F. Chateauneuf, M.-A. Soucy, S. Fortin, "ACE-FTS instrument: after two years on-orbit," Proceedings of Optics & Photonics 2005, San Diego, CA, USA, July 31-Aug. 4, 2005, SPIE Vol. 5883-15

41) P. Bernath, C. Boone, K. Walker, R. Skelton, R. Nassar, S. McLeod, "The Atmospheric Chemistry Experiment (ACE): An Overview," 12th ASSFTS (Atmospheric Science from Space using Fourier Transform Spectrometry) Workshop, May 18-20, 2005, Quebec City, Canada

42) C. R. Nowlan, J. R. Drummond, K. Strong, C. T. McElroy, C. Midwinter, D. S. Turner, "Temperature and Pressure Retrievals from the MAESTRO Space Instrument," Proceedings of IGARSS, Toronto, Canada, Jun. 24-28, 2002

43) C. T. McElroy, "First data from the MAESTRO instrument on the Canadian satellite SciSat-1," Proceedings of SPIE, Earth Observing Systems VIII, Vol. 5151, Aug. 3-6, 2003, San Diego, CA

44) http://www.ace.uwaterloo.ca/data.html
 


The information compiled and edited in this article was provided by Herbert J. Kramer from his documentation of: "Observation of the Earth and Its Environment: Survey of Missions and Sensors" (Springer Verlag) as well as many other sources after the publication of the 4th edition in 2002. - Comments and corrections to this article are always welcome for further updates (herb.kramer@gmx.net).

Spacecraft    Launch    Mission Status    Sensor Complement    Ground Segment    References    Back to top