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After
the final count down, PSLV-C8 lifted off
from the Second Launch Pad (SLP) at SDSC
SHAR at 3:30 pm with the ignition of the
core first stage. The important flight events
included the separation of the first stage,
ignition of the second stage, separation
of the payload fairing at about 116 km altitude
after the vehicle had cleared the dense
atmosphere, second stage separation, third
stage ignition and third stage separation,
fourth stage ignition and fourth stage cut-off.
AGILE was placed in orbit 1370.7 sec after
lift off.
With
a much lighter payload and the low inclination
of the orbit in which AGILE was to be placed,
PSLV-C8 was configured, for the first time,
without the six solid propellant strap-on
motors of the first stage. Also, the propellant
in the fourth stage had been reduced by
about 400 kg compared to the previous PSLV
flight. The core-alone PSLV-C8 had a lift-off
mass of 230 tonne.
PSLV
has emerged as the workhorse launch vehicle
of ISRO with ten consecutively successful
flights so far. Since its first successful
launch in 1994, PSLV has launched eight
Indian remote sensing satellites, an amateur
radio satellite, HAMSAT, a recoverable space
capsule, SRE-1, and six small satellites
for foreign customers into 550-800 km high
polar Sun Synchronous Orbits (SSO). Besides,
it has launched India's exclusive meteorological
satellite, Kalpana-1, into Geosynchronous
Transfer Orbit (GTO). PSLV will also be
used to launch India's first spacecraft
mission to moon, Chandrayaan-1, during 2008.
In
its standard configuration, the 44 m tall
PSLV has a lift-off mass of 295 tonne. It
is a four-stage launch vehicle with the
first and the third stages as well as the
six strap-ons surrounding the first stage
using HTPB based solid propellant. PSLV's
first stage is one of the largest solid
propellant boosters in the world. Its second
and fourth stages use liquid propellants.
PSLV's bulbous payload fairing has a diameter
of 3.2 metre. The vehicle has S-band telemetry
and C-band transponder systems for monitoring
its health and flight status respectively.
It also has sophisticated auxiliary systems
like stage and payload fairing separation
systems.
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