Engineering:SICRAL 1B

From HandWiki
SICRAL 1B
Mission typeCommunications
OperatorTelespazio
MDD, Turkey
COSPAR ID2009-020A
Mission duration13 years
Spacecraft properties
BusItalsat 3000
ManufacturerThales Alenia Space
Launch mass3,038 kilograms (6,698 lb)
Start of mission
Launch date20 April 2009, 08:15:59 (2009-04-20UTC08:15:59Z) UTC
RocketZenit-3SL
Launch siteKiribaty atom test site Odyssey, KBTM
ContractorSea Launch
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Longitude11.8° east
Perigee altitude35,775 kilometres (22,230 mi)
Apogee altitude35,811 kilometres (22,252 mi)
Inclination0.11 degrees
Period23.93 hours
Epoch25 October 2013, 02:29:49 UTC[1]
 

SICRAL 1B is a military communications satellite built by Thales Alenia Space for Italian Armed Forces. It is a dual-use spacecraft: Telespazio will use some of the satellite's transmission capacity and some will be used by the Italian defense ministry and NATO. The spacecraft is based on the Italsat 3000 bus and includes one EHF/Ka band, three UHF-band and five active SHF-band transponders. It is designed to be operable for 13 years.[2]

Construction

Thales Alenia Space was the prime contractor for development and construction of the SICRAL 1B satellite.[3]

Launch

On April 20, 2009 Sea Launch used a Zenit-3SL to carry SICRAL 1B into a geosynchronous transfer orbit. Liftoff from the Ocean Odyssey launch platform took place at 08:16 GMT.[4]

References