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LVM3(Launch Vehicle Mk III)

Introduction

→ The ISRO developed the three-stage heavy lift launch vehicle known as the Geosynchronous Satellite Launch Vehicle, or GSLV (Launch Vehicle Mark III). 

→ The heaviest satellites that can be carried by this launch vehicle include. 

→ The LVM, also known as the GSLV Mk III, was designed with specific objectives in mind. 

→ The page below details these aims as well as the LVM's successful launches, payload capacity, and engines.

💡Table of Content

    ➤  Introduction

GSLV Mk III or LVM Objectives

→ LVM Mk-III has more thrust than the Polar Satellite Launch Vehicle (PSLV), ISRO's most successful launch vehicle. 

→ The following is a list of GSLV Mk III's development goals.

  • to orbit more substantial communication satellites
  • to launch larger, more versatile spacecraft into orbit
  • Travel between planets in the future
  • to begin the launch of impending crewed missions, or space travel.

Vehicle Specifications for the LVM Mk III

  • Height: 43.5 m
  • Vehicle Diameter: 4.0 m
  • Heat Shield (Payload Fairing) Diameter: 5.0 m
  • Number of Stages: 3
  • Lift-Off Mass: 640 tonnes

Technical Specification for LVM Mk III

→ Here is a simplified explanation of Technical Specification
  1. GTO payload: 4,000 kg
  2. LEO (Low Earth Orbit) payload: 8,000 kg
  3. Upper Cryogenic Stage: C25
  4. Boosters for solid rockets: S200
  5. Core Stage: Liquid Stage L110

(1). GTO payload: 4,000 kg

→ The GSAT series' 4-tonne class satellites can be launched into geosynchronous transfer orbits by LVM3.

(2). LEO (Low Earth Orbit) payload: 8,000 kg

→ LVM3's potent cryogenic stage makes it possible to launch large payloads into Low Earth Orbits with an altitude of 600 km.

(3). Upper Cryogenic Stage: C25

→ The largest cryogenic engine in India, the CE-20, which was created and built by the Liquid Propulsion Systems Centre, powers the C25.

  • Cryo Stage Height: 13.5 m
  • Cryo Stage Diameter: 4.0 m
  • Engine: CE-20
  • Fuel: 28 tonnes of LOX + LH2

(4). Boosters for solid rockets: S200

→ The massive amount of thrust needed for takeoff is provided by two S200 solid rocket boosters, which are used by LVM3. 

→ The Vikram Sarabhai Space Centre was where the S200 was created.

  • Booster Height: 25 m
  • Booster Diameter: 3.2 m
  • Fuel: 205 tonnes of HTPB (nominal)

(5). Core Stage: Liquid Stage L110

→ Two Vikas engines created and developed at the Liquid Propulsion Systems Centre power the L110 liquid stage.
  • Stage Height: 21 m
  • Stage Diameter: 4.0 m
  • Engine: 2 x Vikas
  • Fuel: 115 tonnes of UDMH + H2O

Launch of LVM Mk III

→ The GSLV Mk III has been successfully launched numerous times so far. 

→ Below is a list of the items.

  • Launched in December 2014, CARE stands for Crew Module Atmospheric Re-entry Mission.
  • The GSAT-19 Mission was started in June 2017.
  • The GSAT-29 Mission was launched in November 2018.
  • It was a moon expedition called Chandrayaan 2. 2019 saw its premiere.
  • OneWeb: In October 2022, 36 OneWeb satellites were successfully launched by the first LVM3 commercial launch.
  • OneWeb: OneWeb's second official commercial launch. most substantial load ever launched by an LVM3 and ISRO. The project got underway in March 2023.

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