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Second Launch Pad
Second Launch
Pad (SLP): SLP built at SDSC SHAR at Sriharikota is a state-of-the-art
launch complex. SLP uses the integrate-transfer-and-launch
concept. The launch vehicle is integrated inside a permanent building
called Vehicle Assembly Building (VAB). After checkout, it is transported
on rails to the launch pad using a Mobile Launch Pedestal (MLP). The
vehicle is then interfaced with the launch pedestal and fuel-filling
and checkout operations carried out. The launch takes place after
the final countdown. SLP was built by involving Indian industry on a turnkey basis including design and engineering, procurement of systems and sub-systems, fabrication, erection and commissioning of facilities including civil works.
SLP consists of the following major elements: Vehicle Assembly
Building (VAB): It is in this building that the vehicle integration
is carried out on a Mobile Launch Pedestal (MLP) and then the vehicle
transferred to Umbilical Tower for launch after carrying out the total
checkout of the integrated vehicle. The 82 m tall VAB houses a 200
tonne and a 30 tonne capacity cranes for lifting vehicle stages. It
has 20 horizontal sliding doors of varying sizes with the largest
being 13 x 20 m. Six 14 x 6 m foldable and vertically repositionable
platforms at different levels help vehicle integration and servicing.
VAB is equipped with an elevator also. Mobile Launch
Pedestal (MLP): The 19.5 x 19.5 m MLP with a bogie system is used
to transfer the integrated vehicle from VAB to the launch pad located
at a distance of 1 km. With a height of 8.6 m, Umbilical Tower (UT): The 70 m tall, 10 x 10 m UT weighs about 980 tonne. The fully integrated vehicle on MLP, on its arrival on rails, is interfaced with UT with electrical, pneumatic and fluid filling lines. The final operations like fuel filling, gas charging and the vehicle checkout are carried out on UT. It has three platforms, which can be swung and also positioned/moved vertically to different levels. UT has an elevator and a 10 tonne tower crane at the top. It has a cryo arm for cryogenic fuel filling operations and monitoring till the last minute of launch operations.
Jet Deflector:
The jet deflector system is used to move the hot gases, ejected from
the launcher during lift-off, away from the launch pad so as to reduce
the thermal and acoustic loads on the vehicle. The design and construction
of jet deflector was one of the major engineering challenges. It has
diaphragm wall construction with piles driven 45 m below ground, constructed
for the first time on the east coast of India. Lightning Protection Towers: In order to protect the launch vehicle from severe lightning when the vehicle is exposed for longer duration, lightning protection towers are erected around UT. There are four lightening protection towers of 120 m height around UT, which are interconnected through cables.
Propellant
Storage and Servicing Facilities: Propellant storage and servicing
facilities cater to the storage of about 1000 tonne of earth storable
propellants (UDMH and N2O4), cryogenic propellants (liquid Oxygen and
liquid Hydrogen), water, etc. A large gas storage and supply system
to supply the required quantity of Helium for on-board systems and Nitrogen
system for meeting the purging requirements is part of this facility.
A water tank of 5 lakh litre capacity is also included. Utilities:
These include instrumentation and control systems, compressed air and
fire fighting system, overhead tank, water treatment plant, electrical
sub-station, air conditioning plant and safety system. Track
for movement of MLP: MLP with the integrated vehicle moves on a twin
double rail track with a span of Some of the challenges in the establishment of SLP were: overcoming the problems of shallow water table at the site, constructing a jet deflector 45 m below the ground which involved dewatering, pile driving etc., transporation of odd sized heavy structurals, design and fabrication of bogie wheels with each wheel taking a load of up to 175 tonne and construction of a 1 km long rail track with stringent deflection criteria. |