| Mission type | Asteroid detection |
|---|---|
| Operator | CSA,DRDC[1] |
| COSPAR ID | 2013-009D |
| SATCATno. | 39089 |
| Website | neossat |
| Mission duration | Primary mission: 1 year[2] Elapsed: 12 years, 8 months and 30 days |
| Spacecraft properties | |
| Bus | Multi-Mission Microsatellite Bus[3] |
| Manufacturer | David Florida Laboratory,Spectro, Microsat Systems[4] |
| Launch mass | 74 kg (163 lb)[5] |
| Dimensions | 137 × 78 × 38 cm (54 × 31 × 15 in)[5] |
| Power | 45 watts[5] |
| Start of mission | |
| Launch date | February 25, 2013, 12:31 (2013-02-25UTC12:31Z) UTC |
| Rocket | PSLV-CA C20 |
| Launch site | Satish DhawanFLP |
| Contractor | ISRO/Antrix |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Sun-synchronous[6] |
| Semi-major axis | 7,155.78 km (4,446.40 mi)[7] |
| Perigee altitude | 776 km (482 mi)[7] |
| Apogee altitude | 792 km (492 mi)[7] |
| Inclination | 98.61 degrees[7] |
| Period | 100.41 minutes[7] |
| Mean motion | 14.34[7] |
| Epoch | 24, 20, 10:52:44 UTC[7] |
TheNear Earth Object Surveillance Satellite (NEOSSat)[8] is a Canadianmicrosatellite using a 15-cm aperture f/5.88Maksutovtelescope (similar to that on theMOST spacecraft), with 3-axis stabilisation giving a pointing stability of ~2arcseconds in a ~100 second exposure. It is funded by theCanadian Space Agency (CSA) andDefence Research and Development Canada (DRDC),[1] and searches for interior-to-Earth-orbit (IEO)asteroids,[9][10] at between 45 and 55 degreesolar elongation and +40 to -40 degreesecliptic latitude.[3]
NEOSSat is a suitcase-sizedmicrosatellite measuring 137 × 78 × 38 centimetres (54 × 31 × 15 in), including telescopebaffle, and weighing 74 kilograms (163 lb).[5][11] It is powered bygallium arsenide (GaAs)solar cells placed on all six sides of its frame;[5] the entire spacecraft uses around 80 watts of power,[12] with thebus core systems consuming an average of 45 watts.[5] The spacecraft uses miniaturereaction wheels for stabilization and attitude control,[13][14] andmagnetic torque rods to dump excess momentum by pushing against Earth's magnetic field,[13][5] so no on-board fuel is required for operation.[14]
NEOSSat is a descendant of Canada's earlierMOST satellite. It was built on the Multi-Mission Microsatellite Bus, which was created using data from the development of MOST.[10] Its science payload includes a telescope of the same design as that on MOST,[3][6] and uses spareCCD detectors from the MOST mission.[6]
The sole instrument is a 15-centimetre (5.9 in)Rumak-Maksutov telescope with a 0.86degreefield of view and af/5.88focal ratio.[5] Incoming light is split and focused on two passively cooled 1024×1024 pixel CCDs,[5] one used by the NESS and HEOSS projects and the other by the spacecraft'sstar tracker.[13] Since the telescope is aimed relatively close to the Sun, it contains a baffle to shield its detectors from intense sunlight.[6] The science camera takes 100-second-long exposures, allowing it to detect celestial objects down tomagnitude 20.[6] NEOSSat's attitude control allows it to maintainpointing stability of less than onearcsecond during the entire 100 second exposure period.[5][14] It takes up to 288 images per day,[6] downloading multiple images to its Canadian ground station with each pass.[10]
NEOSSat was originally scheduled for launch in 2007,[15] but delays set it back until 2013.[16] Alongside another Canadian spacecraft,Sapphire (a military surveillance satellite), and five other satellites, NEOSSat launched on February 25, 2013, from theSatish Dhawan Space Centre inSriharikota, India, at 12:31UTC aboard an IndianPSLV-C20 rocket.[17][18]
The NEOSSat satellite carries out three missions.
The spacecraft is a demonstrator of the utility of theMulti-Mission Microsatellite Bus (MMMB) as part of the CSA's efforts to develop an affordable multi-mission bus.[19][20]
Near Earth Space Surveillance (NESS),[8] led by Principal InvestigatorAlan Hildebrand of the University of Calgary, uses NEOSSat to search for and track near-Earth asteroids inside Earth's orbit around the Sun, including asteroids in theAten andAtira classes. These asteroids are particularly difficult to detect from the surface of the Earth, as they are usually positioned in the daylit or twilit sky, when background light from the Sun makes such faint objects invisible. This form of stray light is not an issue for a telescope in orbit, making even a small-aperture telescope such as that on NEOSSat capable of detecting faint asteroids. The NESS science team expects to be able to detect many such asteroids as faint as visual magnitude 19. The NESS mission is funded by the CSA.
High Earth Orbit Space Surveillance (HEOSS),[21] led by Principal Investigator Brad Wallace of DRDC, uses NEOSSat to conduct experimental satellite tracking activities. It focuses principally on satellites in the 15,000 to 40,000 km (9,300 to 24,900 mi) range,[19] such as geostationary communications satellites, which are difficult to track via ground-based radar. These experiments include submitting tracking data to theSpace Surveillance Network, as part of Canada's role inNORAD. The HEOSS activities support planning for follow-on missions to the Canadian Department of National Defence's operational satellite-tracking satellite,Sapphire, which was launched with NEOSSat. The HEOSS mission is funded by DRDC.
NEOSSat, originally conceived under the name NESS ("Near Earth Space Surveillance"),[22] was proposed by Dynacon in 2000 to DRDC and CSA as a follow-on to theMOST microsatellite mission which was then halfway through its development. As conceived during an initial Phase A study for DRDC, it would have re-used almost all of the equipment designs from MOST, the main addition being a large external baffle to reduce the stray light impinging on the instrument's focal plane, necessary in order to achieve its asteroid detection sensitivity target of magnitude 19.
DRDC's Technology Demonstration Program (TDP) approved CDN$6.5M of funding for NEOSSat in 2003. By mid-2004 CSA had approved the remaining funding needed to initiate the NEOSSat procurement, and with DRDC formed a Joint Program Office to manage the mission development.[15] At this point the spacecraft's name was changed from NESS to NEOSSat. A final Phase A study was carried out under CSA supervision in 2005, and a Phase B/C/D procurement was carried out in 2006/07, with a total development price cap of CDN$9.8M (not including launch cost). Dynacon was selected as prime contractor in 2007, at which point the total development cost was reported as CDN$11.5M, with a target launch date of late 2009.[23] Shortly after that, Dynacon sold its Space division to Microsat Systems Canada Inc. (MSCI), which completed development of NEOSSat.
As development proceeded, while the basic design concept was kept, much of the equipment in the satellite was replaced by new designs in order to meet requirements imposed by the CSA's Multi-Mission Microsatellite Bus program.[21] The basic instrument design was kept, as was the basic structure design, and the attitude control subsystem sensors and actuators; the on-board computers and radios were replaced, the instrument readout electronics was redesigned, and the external instrument "door" was replaced by an internal shutter.
By 2012, the CSA's contribution to program funding had risen by CDN$3.4M to CDN$8.8M, implying a total program contracted-out cost to end of satellite commissioning of CDN$15.4M.[24] However, according to a Canadian Space Agency audit, the total program cost by the end of 2013 was CDN$25M, including both CSA and DRDC costs, with CSA's portion of the cost reported at just under CDN$13M.[25]
In February 2014, the CSA released a report detailing the results of an audit of the NEOSSat program, commissioned by CSA and conducted by external companies.[25] This audit, carried out as "a requirement of the CSA five-year evaluation plan", covers only the period beginning with the signing of the CSA's NEOSSat contracts in 2005 through the end of 2013.[25] Reports highlighted several negative findings of the audit, including delays in the program, and problems experienced by the satellite on-orbit that have kept it from achieving operational status. This includes the Electrical Power Subsystem interfering with the imager CCD, and delays in the development of flight software needed for operating the camera and maintaining spacecraft pointing stability.[20] These problems were mainly attributed to poor performance by the contractor, MSCI, as well as to a perception that the project had been "under-funded by as much as 50 per cent" from the outset.[26] However, MSCI has disputed criticism against the company, saying that program requirements were poorly written and that CSA staff interfered with the satellite's construction.[27]
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