Engineering:Radarsat-1

RADARSAT-1

RADARSAT-1 satellite
Mission type	Earth observation
Operator	Canadian Space Agency
COSPAR ID	1995-059A
SATCAT no.	23710
Website	www.asc-csa.gc.ca/eng/satellites/radarsat1/
Mission duration	5 years (planned) 17 years, 4 months, 24 days (achieved)
Spacecraft properties
Bus	RADARSAT
Manufacturer	MDA (formerly Spar Aerospace) Ball Aerospace
Launch mass	2,750 kg (6,060 lb)
Power	2.1 kW
Start of mission
Launch date	4 November 1995, 14:22 UTC
Rocket	Delta II 7920-10
Launch site	Vandenberg, SLC-2W
Contractor	Boeing
End of mission
Last contact	29 March 2013
Orbital parameters
Reference system	Geocentric orbit
Regime	Low Earth orbit
Perigee altitude	793 km (493 mi)
Apogee altitude	821 km (510 mi)
Inclination	98.60°
Period	100.70 minutes
RADARSAT constellation

RADARSAT-1 was Canada's first commercial Earth observation satellite. It utilized synthetic aperture radar (SAR) to obtain images of the Earth's surface to manage natural resources and monitor global climate change. As of March 2013, the satellite was declared non-operational and is no longer collecting data.

Mission

RADARSAT-1 was launched at 14:22 UTC on 4 November 1995, from Vandenberg Air Force Base in California , into a Sun-synchronous orbit (dawn-dusk) above the Earth with an altitude of 798 km (496 mi) and inclination of 98.60°. Developed under the management of the Canadian Space Agency (CSA) in co-operation with Canadian provincial governments and the private sector, it provided images of the Earth for both scientific and marketing purposes. RADARSAT-1's images were useful in many fields, including agriculture, cartography, hydrology, forestry, oceanography, geology, ice and ocean monitoring, arctic surveillance, and detecting ocean oil slicks.

History

The Canadian Space Agency (CSA) RADARSAT-1 project was conceived in the early 1980s and included discussions with NASA.

NASA provided the Delta II launch vehicle to launch RADARSAT-1 and access to the NASA Deep Space Network (NASA DSN) in exchange for access to its data. Estimates are that the project, excluding launch, cost CA$620 million. The Canadian federal government contributed about CA$500 million, the four participating provinces (Québec, Ontario, Saskatchewan and British Columbia) about CA$57 million, and the private sector about CA$63 million.

RADARSAT International, Inc. (RSI), a Canadian private company, was created in 1989 to process, market and distribute RADARSAT-1 data. (RADARSAT International, Inc. (RSI) was later acquired by MacDonald Dettwiler and Associates.) In 2006, RSI was rebranded MDA Geospatial Services International or MDA GSI.

Payload

RADARSAT-1 used a synthetic aperture radar (SAR) sensor to image the Earth at a single microwave frequency of 5.3 GHz, in the C band (wavelength of 5.6 cm). The SAR support structure was designed and manufactured by Northrop Grumman Astro Aerospace and deployed to 15 m (49 ft) in length on orbit. Unlike optical satellites that sense reflected sunlight, SAR systems transmitted microwave energy towards the surface and recorded the reflections. Thus, Radarsat-1 imaged the Earth, day or night, in any atmospheric condition, such as cloud cover, rain, snow, dust or haze.

Each of RADARSAT-1's seven beam modes offered a different image resolution. The modes included Fine, which covers an area of 50 × 50 km (31 × 31 mi) (2,500 km² (970 sq mi)) with a resolution of 10 m (33 ft); Standard, which covered an area of 100 × 100 km (62 × 62 mi) (10,000 km² (3,900 sq mi)) and had a resolution of 30 m (98 ft); and ScanSAR wide, which covered a 500 × 500 km (310 × 310 mi) (250,000 km² (97,000 sq mi)) area with a resolution of 100 m (330 ft). RADARSAT-1 also had the unique ability to direct its beam at different angles.

Orbit

Orbital trace of Radarsat-1

With an orbital period of 100.70 minutes, RADARSAT-1 circles the Earth 14 times a day. The orbit path repeats every 24 days, this means that the satellite is in exactly the same location and could take the same image (same beam mode and beam position) every 24 days. This is useful for interferometry and detecting changes at that location that took place during the 24 days. Using different beam positions, a location can also be scanned every few days.

RADARSAT-1 was a right-looking satellite, meaning that the microwave beam transmits and receives on the right side of the satellite, relative to its orbital path. As it descends in its orbit from the North Pole, it faces west, and when it ascends from the South Pole, it faces east. Locations could therefore be imaged from opposite sides. Combined with the different beam modes and positions, this provided users with many possible perspectives from which to image a location.

End of service

On 4 November 2010, RADARSAT-1 celebrated its 15-year service anniversary. It outlived its planned five-year lifetime by a wide margin. Radarsat-2 was launched on 14 December 2007 from Baikonur, Kazakhstan

RADARSAT-1 covered the Arctic daily, and most of Canada every 72 hours depending on instrument orientation and mode. It covered the entire Earth every 24 days.

On 29 March 2013, RADARSAT-1 experienced a technical problem. The Canadian Space Agency (CSA) assembled a team of engineers, who conducted an extensive investigation. Following numerous attempts to resolve the problem, the CSA, in consultation with its commercial data distributor MDA Geospatial Services Inc. concluded that RADARSAT-1 was no longer operational.

See also

• RADARSAT-2
• RADARSAT Constellation

External links

• RADARSAT-1 from the CSA