Launch
Vehicles are used to transport and
put satellites or spacecrafts into space. In India,
the launch vehicles development
programme began in the early 1970s.
The first experimental Satellite
Launch Vehicle (SLV-3) was developed
in 1980. An Augmented version of
this, ASLV, was launched successfully
in 1992. India has made tremendous
strides in launch vehicle technology
to achieve self-reliance in satellite
launch vehicle programme with the
operationalisation of Polar Satellite
Launch Vehicle (PSLV) and Geosynchronous
Satellite Launch Vehicle (GSLV).
PSLV represents ISRO's first attempt to design and develop an
operational vehicle that can be used to orbit application satellites. While
SLV-3 secured for India a place in the community of space-faring nations, the
ASLV provided the rites of passage into launch vehicle technology for ISRO. And
with PSLV, a new world-class vehicle has arrived. PSLV has repeatedly proved
its reliability and versatility by launching 53 satellites / spacecrafts ( 26
Indian and 27 Foreign Satellites) into a variety of orbits so far.
Landmark achievents in ISRO's Launch Vehicle
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ISRO's Launch Fleet at a Glance
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Satellite Launch Vehicle-3 (SLV-3), India's first
experimental satellite launch vehicle was successfully launched on July 18,
1980 from SHAR Centre Sriharikota, when Rohini satellite, RS-1, was placed in
orbit. SLV-3 was a 22 m long, all solid, four stage vehicle weighing 17 tonnes
capable of placing 40 kg class payloads in low earth orbit.
It employed an open loop guidance (with stored pitch programme) to steer the vehicle in flight along pre-determined trajectory. The first experimental flight of SLV-3, in August 1979, was only partially successful. Apart from the July 1980 launch, there were two more launches held in May 1981 and April 1983,orbiting Rohini satellites carrying remote sensing sensors.
It employed an open loop guidance (with stored pitch programme) to steer the vehicle in flight along pre-determined trajectory. The first experimental flight of SLV-3, in August 1979, was only partially successful. Apart from the July 1980 launch, there were two more launches held in May 1981 and April 1983,orbiting Rohini satellites carrying remote sensing sensors.
Augmented Satellite Launch Vehicle (ASLV) was developed to
act as a low cost intermediate vehicle to demonstrate and validate critical
technologies. With a lift off weight of 40 tonnes, the 23.8 m tall ASLV was
configured as a five stage, all-solid propellant vehicle, with a mission of
orbiting 150 kg class satellites into 400 km circular orbits. The strap-on
stage consisted of two identical 1m diameter solid propellant motors, Under the
ASLV programme four developmental flights were conducted.
The first developmental flight took place on March 24, 1987 and the second on July 13, 1988. ASLV-D3 was successfully launched on May 20, 1992, when SROSS-C (106 kg) was put into an orbit of 255 x 430 km. ASLV-D4, launched on May 4, 1994, orbited SROSS-C2 weighing 106 kg. It had two payloads, Gamma Ray Burst (GRB) Experiment and Retarding Potentio Analyser (RPA) and functioned for seven years. ASLV provided valuable inputs for further development.
The first developmental flight took place on March 24, 1987 and the second on July 13, 1988. ASLV-D3 was successfully launched on May 20, 1992, when SROSS-C (106 kg) was put into an orbit of 255 x 430 km. ASLV-D4, launched on May 4, 1994, orbited SROSS-C2 weighing 106 kg. It had two payloads, Gamma Ray Burst (GRB) Experiment and Retarding Potentio Analyser (RPA) and functioned for seven years. ASLV provided valuable inputs for further development.
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