- Marcopolo
Marcopolo or Marco Polo 1 and 2 were two satellites designed, launched and tested by
Hughes Space and Communications (now part ofBoeing Satellite Systems ) forBritish Satellite Broadcasting , and were used for Britain'sDirect Broadcast Service . [ [http://www.boeing.com/defense-space/space/bss/factsheets/376/bsb/bsb.html BSB History by Boeing] ] Marcopolo 1 launched onAugust 27 ,1989 on the 187th launch of a Delta rocket, and Marcopolo 2 onAugust 17 ,1990 , by a Delta II rocket. [cite web | url = http://www.boeing.com/defense-space/space/bls/missions/index.html | title = Boeing Launch Services Mission Record | publisher = Boeing] Marcopolo I had a Hughes designation as HS376. [ [http://www.nasm.si.edu/research/arch/findaids/pdf/Desind_Finding_Aid.pdf] NASM's Herbert Stephen Desind Collection,p.36]Although the satellites worked perfectly, BSB [ [http://www.tbs-satellite.com/tse/online/sat_bsb_1.html BSB1] ] was a commercial failure and the satellites were sold off and renamed.
Marcopolo 1 was sold off in December
1993 toNordic Satellite AB of Sweden and operated until 2000 as Sirius 1 at 5°E. It was then moved to 13°W, and renamed Sirius W, although it is not currently transmitting any services.Marcopolo 2 was sold in July
1992 toTelenor of Norway and renamed Thor 1. It was located at 0.8°W until it was switched off in January 2002. In November 2002, it was moved to 7.4°W and reactivated with digital test signals broadcasting towards Scandinavia. Marcopolo 2 was sent up to thejunk orbit in early January 2003.pecifications [ [http://www.tbs-satellite.com/tse/online/prog_bsb_car.html BSB Specs] ]
*Prime contractor: Hughes
*Platform: HS-376
*Mass at launch: 1250 kg
*Mass in orbit: 660 kg
*Payload mass: 100 kg: transponders: 90 kg, antennas: 10 kg
*Diameter: 2.16 m
*Height: 2.7 m (7.2 m deployed)
*Stabilization: Spin stabilized
*DC power: BOL: 1024 W
*Design lifetime: 10 years
*Beacon: 12.494 or 12.495 GHzReferences
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