SECOND ROCKET LAUNCH PAD – SCI & TECH

News: Honourable Prime Minister Lays the Foundation Stone for India's Second Spaceport

 

What's in the news?

       In a momentous occasion for India's space ambitions, Hon’ble Prime Minister Shri Narendra Modi remotely laid the foundation stone for India's second spaceport at Kulasekharapattanam, a coastal village in Tamil Nadu's Thoothukudi district.

 

Key takeaways:

       The selection of Kulasekarapattinam offers strategic advantages, particularly in enhancing payload capability with its direct southward launch trajectory for small launch vehicles.

 

Second Rocket Launch Pad:

       It is a new spaceport coming up at Kulasekarapattinam, a coastal hamlet near the temple town of Tiruchendur in Thoothukudi district in southern Tamil Nadu.

       Exclusively serve the private sector, with no ISRO rocket launches planned from there.

       It will be second after the space agency’s existing Satish Dhawan Space Centre, founded in Andhra Pradesh’s Sriharikota in 1971, with two launch pads.

 

Features:

       It will focus on the launch of Small Satellite Launch Vehicles (SSLVs) on a commercial basis.

       It will house 35 facilities, including a launch pad, rocket integration facilities, ground range and checkout facilities, and a mobile launch structure (MLS) with checkout computers.

       It would have the capacity to launch 24 satellites per year using a mobile launch structure.

 

Why Tamil Nadu?

       Allowing for direct southward trajectories ideal for launches using the Small Satellite Launch Vehicle (SSLV).

       Kulasekharapatnam space port will help save fuel for small rocket launches as the port can launch rockets directly south over the Indian Ocean without requiring crossing landmasses.

       This is unlike the existing launch site at the Satish Dhawan Space Centre, which adds more fuel requirements for launching into a polar orbit as rockets need to follow a curved path to the south to avoid Sri Lanka’s landmass.

       Equatorial Proximity:

       Closer proximity to the equator enhances the velocity imparted by Earth's rotation, leading to increased payload capacity for launch vehicles, particularly beneficial for geostationary satellites.

       Dogleg manoeuvre:

       It is a sharp turn that causes the rocket to deviate from a straight flight path.

       This manoeuvre requires more fuel in the rocket which eats into the payload capacity of the launcher

 

Go back to basics:

Small Satellite Launch Vehicles:

       SSLV is a 3-stage Launch Vehicle configured with three Solid Propulsion Stages and liquid propulsion-based Velocity Trimming Module (VTM) as a terminal stage.

       SSLV is 2m in diameter and 34m in length with lift off weight of 120 tonnes.

       SSLV is capable of launching 500kg satellite in 500 km planar orbit.

       The key features of SSLV are Low cost, with low turn-around time, flexibility in accommodating multiple satellites, Launch on demand feasibility, minimal launch infrastructure requirements