The Indian Space Research Organisation (ISRO) has successfully launched the GSAT-7R (CMS-03)  communication satellite aboard the LVM-3 M5 (Launch Vehicle Mark-3) for the Indian Navy.

• The previous mission of LVM3 launched the Chandrayaan-3 mission, where India became the first country to land successfully near the lunar south pole.

About GSAT-7R(CMS-03)

• It is a part of India’s advanced defence communication satellite series GSAT-7.
• Launch Vehicle: Launch Vehicle Mark 3 (LVM3) 
• Launch Site: Satish Dhawan Space Centre (SDSC-SHAR), Sriharikota
• Orbit: The GSAT-7R (CMS-03) satellite was placed into a Geosynchronous Transfer Orbit (GTO) with an elliptical orbit approximately 250 km at perigee and 29,970 km at apogee. 
  • From this orbit, it will gradually use its onboard propulsion to reach its final Geostationary Orbit, approximately 35,786 kilometers above Earth.
  • A GTO is an elliptical orbit used to transfer a satellite from low Earth orbit (LEO) to a geosynchronous orbit (GEO).
• Weight: Approximately 4,400 kg, making it the heaviest communication satellite launched from Indian soil.
  • The GSAT-11 launched in 2018 weighed over 5,800 kg but had used the European Ariane-5 rocket.
• Purpose: Replacement for the ageing GSAT-7 (2013) to strengthen the Indian Navy’s secure communication network over the Indian Ocean Region (IOR).
• Coverage: Provides real-time, encrypted communication over the entire Indian landmass and adjoining maritime zones.
• Operational Life: Designed for a 15-year service life.
• Payload Features: Equipped with multiband transponders supporting voice, video, and data services with high-bandwidth connectivity.
• Applications: Facilitates real-time communication, disaster management coordination, and support for naval and coastal security operations.

Significance of the CMS-03 Launch

• Indigenous Capability for Heavy Satellites: 
  • Until now, India’s heavier communication satellites such as GSAT-11 (5,854 kg) and GSAT-24 (4,181 kg) were launched by ArianeSpace, and GSAT-20 (4,700 kg) by SpaceX.
  • CMS-03 launch marks India’s transition to self-reliance in heavy satellite deployment.
• Orbit Optimization:
  • To accommodate the 4,410 kg payload (slightly above LVM3’s standard GTO capacity), ISRO adjusted the GTO’s apogee to 29,970 km instead of 36,000 km.
  • Demonstrates adaptive mission planning to maximize payload capacity.
• Platform for Future Missions Support: The LVM3 vehicle family will serve as the launch vehicle for Gaganyaan, India’s first crewed space mission.

Strategic and Economic Implications

• Strategic Autonomy: Reduces India’s dependency on foreign space launchers for heavy satellites.
  • ISRO had been relying on the European rocket for sending all its heavier satellites, weighing more than 3,000 kg.
• Economic Competitiveness: Positions India competitively in the global commercial launch market, currently dominated by SpaceX, Arianespace, and China.
• Human Spaceflight Capability: Paves the way for Gaganyaan and space station missions.
• Technological Innovation: Advances in cryogenic propulsion, semi-cryogenic engines, and reusable launch systems will enhance India’s long-term space competitiveness

About Launch Vehicle Mark-3 (LVM3)

• Overview: LVM3, nicknamed “Bahubali”, is India’s most powerful operational rocket, developed by ISRO for launching heavy communication satellites and interplanetary missions.
• Formerly Known As: Geosynchronous Satellite Launch Vehicle Mark-III (GSLV Mk-III).
• Capability: Designed to carry communication, navigation, and deep-space missions (like Chandrayaan & Gaganyaan).
• Type: Three-stage rocket using solid, liquid, and cryogenic fuel engines.
• Stages:
  • Stage 1 – Solid Propellant – Two large strap-on boosters for liftoff
  • Stage 2 – Liquid Propellant – Provides initial thrust after boosters separate
  • Stage 3 – Cryogenic (Liquid Hydrogen + Liquid Oxygen) – Final stage which injects satellite into orbit
• Payload Capacity:
  • Up to 8,000 kg to Low Earth Orbit (LEO) (~2,000 km altitude).
  • Up to 4,000 kg to Geosynchronous Orbit (GEO) (~36,000 km altitude).
• Major Achievements:
  • Successfully launched Chandrayaan-2 (2019) and Chandrayaan-3 (2023).
  • Conducted Crew Module Atmospheric Re-entry Test (2014) — key for Gaganyaan.
  • Carried out OneWeb missions (2022–23) to LEO after the Russia–Ukraine war halted OneWeb’s international launch options.
• Rebranding: Renamed as LVM3 after demonstrating versatility beyond GEO missions (e.g., 5,700 kg payload for OneWeb to 450 km orbit).

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Upgradation Plans

ISRO is actively enhancing LVM3’s thrust and efficiency for future deep-space and human missions.

• Cryogenic Stage Enhancement (C25 → C32):
  • The current C25 cryogenic upper stage carries 28,000 kg of propellant, producing 20 tonnes of thrust.
  • The new C32 stage under development will carry 32,000 kg propellant and produce 22 tonnes of thrust — increasing payload capacity.
• Semi-Cryogenic Engine Development:
  • Plan to replace the liquid-fuel-based second stage with a semi-cryogenic engine (liquid oxygen + refined kerosene).
  • Expected Benefits: 
    • Increased efficiency and thrust.
    • Lower cost and higher reusability potential.
    • Payload capacity could increase from 8 tonnes to ~10 tonnes in LEO.
• Future Applications:
  • LVM3’s upgraded version could carry the first module of the Bharatiya Antariksh Station (BAS).
  • ISRO is also designing a new Lunar Module Launch Vehicle (LMLV) with a payload capacity of up to 80,000 kg to LEO for future lunar and human missions.

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