Union cabinet approves the establishment of ‘Third Launch Pad’ (TLP) project | Current Affairs | Vision IAS
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The project will be established at Satish Dhawan Space Centre of ISRO at Sriharikota, Andhra Pradesh.

About TLP

  • Key features: Configured to support Launch of NGLV and Launch Vehicle Mark-3 (LVM3) vehicles with Semi cryogenic stage.
    • Supports horizontal & tilted integration of New NGLVs
  • Significance: Enables higher launch frequencies and enhances the launch capacity for future human spaceflight & space exploration missions etc.  

Existing launch pads in India 

  • Currently, ISRO relies on 2 launch pads located at Shriharikota - First Launch Pad (FLP) & Second Launch Pad (SLP).
    • FLP was realized for Polar Satellite Launch Vehicle (PSLV) and continues to provide launch support for PSLV & SSLV.
    • SLP was established primarily for GSLV & LVM3 and also functions as standby for PSLV.
      • Launched the Chandrayaan-3 mission & set to launch the Gaganyaan missions.   

Reasons for Selecting Sriharikota for TLP: 

  • Located on eastern coast: Facilitates the launching in an easterly direction, taking advantage of earth’s rotation.
  • Proximity to equator: Provides launch vehicles with an additional push (Earth's rotation from west to east is fastest at equator) leading to substantial increase in pay loads & cutting down the operational costs.
  • Safety Purpose: Does not have major international maritime or airline routes crisscrossing testing.
  • Others: Largely uninhabited area & closer to the sea ensuring flight path of launch vehicles is entirely over the sea etc. 

New Generation Launch Vehicles (NGLV) Programme  

  • About: Programme by ISRO to develop a new rocket (also known as Soorya Rocket) to launch satellites, spacecraft and other payloads.
  • Features:
    • 3 stage vehicle with reusable first stage. Reusability results in low-cost access to space and modular green propulsion systems.  
    • The booster stages will use semi-cryogenic propulsion, using refined kerosene as fuel and liquid oxygen (LOX) as oxidizer.
    • It will have 3 times the present payload capability with 1.5 times the cost compared to LVM3.
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