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IN THE NEWS
April 18th 2008 Update:
An
Arianespace
Ariane-5 ECA is scheduled to liff off at 22:17 UTC/GMT
today
from Guiana Space Center in Kourou, French Guiana.
The Ariane-5 ECA will deliver both Vietnam's Vinasat-1
and Brazil's Star One C2 telecommunications satellites
into geostationary transfer orbits.
The Ariane-5 ECA is a latest
version of the Ariane-5 launcher. It is designed to
handle dual launches of very large satellites and place
payloads weighing up to 9.6 tonnes into geostationary
transfer orbit.
The Launch is completed and
successful [VIDEO VIEW]
April 12th 2008 News (VINASAT-1 Installed on Ariane-5
for April 18 Launch)
VINASAT-1 is now positioned on Ariane-5's cryogenic core
stage during integration activity inside the Final
Assembly Building. This Lockheed Martin-built spacecraft
is Vietnam's initial telecommunications satellite, and
it will ride as the lower passenger in Ariane-5's
dual-payload "stack" during the April 18 launch.
March 2008 News (Vietnam's
VINASAT-1 satellite is readied for Arianespace's
heavy-lift Ariane 5 mission in April):
Vinasat is now on the
Kourou launch pad in French Guyana and is scheduled to
be shot into orbit on 12 April 2008. It will circle the
earth at 132 degrees east, a position that Vietnam
registered with the International Telecommunications
Union (ITU) in 1999. Vinasat will be operated by
incumbent telco Vietnam Post and Telecoms (VNPT)’s
international telephony arm Vietnam Telecom
International (VTI). Vinasat will be able to provide
more than 200 digital television channels and tens of
thousands of data transmission and telephone channels.
2007 News:
The Vietnamese Government decided May 2008
is the deadline for launching the first Vietnam's
communication satellite into orbit . It's the medium-sized satellite coded
"Vinasat". The Vinasat will span its coverage over Vietnam,
other Southeast Asian countries such as Japan, the Korean
peninsula, Eastern Oceania and South China Sea. The U.S.
based company Lockheed-Martin Commercial Space Systems
won a 180 million USD bid in May 2006 (contract
signed May 12, 2006 in Hanoi) to build and
launch the Vinasat for Vietnam.

Details information of Vinasat-1:
Nation: Vietnam
Type / Application: Communication
Operator: Vietnam Posts and Telecommunications Group (VNPT)
of Vietnam
Contractors: Lockheed-Martin
Equipment: C- and Ku-band transponders
Configuration:
A2100A
Propulsion: LEROS-1C
Lifetime: 15 years
Mass 2600 kg
Launch Vehicle: Ariane-5
Orbit: GEO
What is the A2100A Configuration and its Reliability?
The Lockheed Martin
A2100
geosynchronous spacecraft series is designed to meet
a wide variety of telecommunications needs including
Ka-band broadband and broadcast services, fixed
satellite services in C-band and Ku-band payload
configurations, high-power direct broadcast services
using the Ku-band frequency spectrum, and mobile
satellite services using UHF, L-band and S-band
payloads. The A2100's modular design features a
reduction in parts, simplified construction, increased
on-orbit reliability and reduced weight and cost. The company has standardized on this
bus. Much of the R&D is directed toward increasing the
power available on the satellite and the A2100 bus,
which is capable of generating 15 kW in its standard
configuration. This involves work on the integration of
new, higher efficiency solar cells, onto the innovative
solar "pleated shades," the use of high efficiency,
radiation cooled TWTAs, the design of more efficient
heat pipes and fold out radiators and improved design
for thermal dissipation. Company engineers make
extensive use of CAD tools and claim that they can
deliver a satellite that uses the A2100 bus in 18 months
after receipt of the order. The A2100 series is modular and can be
configured in three different sizes:
-
A2100A
= 1 to 4 kW
-
A2100AX = 4 to x kW
-
A2100AXS = Enhanced A2100AX
-
A2100AXX = Stretched version for
mobile communications
-
A2100M =
Military version.
A2100
Reliability Info.:
The A2100
model which had failed in the operation:
: 1998 -
two of five panels on one solar array have not
unfolded, later fuel system problems - partial loss
Nimiq 2: 2003 - power
loss - reduced performance
Telkom 1: 1999 -
solar array drive problems - no performance loss
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