GSLV MK3 Full Form

What is the full form of GSLV MK3?

The full form is Geosynchronous Satellite Launch Vehicle MK3. It is an Indian expendable launch system developed by the Indian Space Research Organization (ISRO). The geostationary satellite launcher has been operating since 2001 and has launched numerous satellites into orbit.

Information about GSLV MK 3:

The GSLV MK3 project was approved in 2002 to achieve the ability to launch a 4-tonne satellite into geostationary orbit, starting with an in-house design. Vehicle. The development program was completed with three successful flights of the LVM3 X, GSLV MkIII D1 and GSLV MkIII D2. A three-tiered GSLV MkIII. A vehicle equipped with two solid fuel external engines (S200), one liquid core stage (L110) and a high thrust cryogenic upper stage (C25). The S200 reliable propellant engine is one of the world's most prominent solid propellant boosters, with 204 tonnes of solid fuel. The L110 liquid stage uses a twin-fluid engine with 115 tonnes of liquid fuel. The C25 upper cryogenic stage is equipped with a proprietary high-thrust cryogenic engine (CE20) with a fuel payload of 28 tonnes.

Characteristics of GSLV MK 3:

• The carrying capacity of the GTO is 4.3 tons.

• Payload capability to support 10-ton missions in low earth orbit (LEO)

• cost-effective

• Reliability improvement, redundant state management

• Potential for future payload growth with minimal design changes

• Supports human-crewed missions of the Indian Space Program.

The objective of GSLV MK 3:

The GSLV MK3 adds a feather to ISRO's remarkable achievement to date. This has strengthened India's position in space technology. GSLV MK 3 achieves multiple goals:

• Heavier satellites weighing up to 10,000 Kg can be launched into lower earth orbits (LEO) of 600 km altitude.

• Payloads of 4,000 kg can now be placed in the Geosynchronous Transfer Orbit (GTO).

• The spacecraft's primary use is to launch communications satellites, which India previously relied on other space agencies.

• It's for ISRO's future manned spaceflight.

Three Stages of GSLV MK 3

GSLV MK 3 The GSLV MK 3 has a 3-stage trigger system:

• Stage 1 - solid propellant stage С200 In the first stage, the rocket is launched using two rocket boosters that use 200 tons of solid fuel.

• Stage 2 - Liquid Fuel Stage L110 This stage uses 110 tons of liquid fuel O. This liquid fuel is a mixture of nitrogen tetroxide and asymmetric dimethylhydrazine.

• Stage 3- Cryogenic Fuel Stage C25 This stage will use India's largest cryogenic engine, using 25 tonnes of a mixture of hydrogen and oxygen.

Payload Capacity of the GSLV Mk III

• It is intended to launch 4 tonnes worth of satellites into geosynchronous transfer orbit (GTO).

• It is capable of launching satellites up to 10 tonnes into Low Earth Orbit (LEO), which is 600 km high.

Engines and Boosters for the GSLV Mk III

• The Core Stage is powered by 2 Vikas Engines. The ISRO Liquid Propulsion Systems Center created these engines.

• A massive thrust is provided to the GSLV Mk III by S 200, 2 Solid Boosters. Vikram Sarabhai Space Centre (VSSC), Trivandrum, created S 200.

• Cryogenic stage refers to the upper stage (C-25). The CE-20, the largest cryogenic engine produced by ISRO, powers this stage. Few countries have created the extremely complicated technology known as cryogenic engines.