The Geosynchronous Satellite Launch Vehicle (GSLV) uses three types of fuel in its operations:

1. Solid fuel: The first stage of the GSLV, also known as the GS1, uses a solid propellant. This is a composite of fine Ammonium Perchlorate (NH4ClO4) powder, acting as the oxidizer, and atomized aluminium powder, which acts as the fuel.

2. Liquid fuel: The second stage of the GSLV, also known as the GS2, uses a liquid propellant. This consists of Unsymmetrical Dimethylhydrazine (UDMH) as fuel and Nitrogen tetroxide (N2O4) as the oxidizer.

3. Cryogenic fuel: The third stage of the GSLV, also known as the GS3 or Cryogenic Upper Stage (CUS), uses cryogenic propellants. This includes Liquid Oxygen (LOX) as the oxidizer and Liquid Hydrogen (LH2) as the fuel. Cryogenic engines provide more thrust for every kilogram of propellant they burn compared to solid and earth-storable liquid propellant rocket stages.

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The Geosynchronous Satellite Launch Vehicle (GSLV) uses three types of fuel in its operations:

1. Solid fuel: The first stage of the GSLV, also known as the GS1, uses a solid propellant. This is a composite of fine Ammonium Perchlorate (NH4ClO4) powder, acting as the oxidizer, and atomized aluminium powder, which acts as the fuel.

2. Liquid fuel: The second stage of the GSLV, also known as the GS2, uses a liquid propellant. This consists of Unsymmetrical Dimethylhydrazine (UDMH) as fuel and Nitrogen tetroxide (N2O4) as the oxidizer.

3. Cryogenic fuel: The third stage of the GSLV, also known as the GS3 or Cryogenic Upper Stage (CUS), uses cryogenic propellants. This includes Liquid Oxygen (LOX) as the oxidizer and Liquid Hydrogen (LH2) as the fuel. Cryogenic engines provide more thrust for every kilogram of propellant they burn compared to solid and earth-storable liquid propellant rocket stages.

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The Geosynchronous Satellite Launch Vehicle (GSLV) uses three types of fuel in its operations:

1. Solid fuel: The first stage of the GSLV, also known as the GS1, uses a solid propellant. This is a composite of fine Ammonium Perchlorate (NH4ClO4) powder, acting as the oxidizer, and atomized aluminium powder, which acts as the fuel.

2. Liquid fuel: The second stage of the GSLV, also known as the GS2, uses a liquid propellant. This consists of Unsymmetrical Dimethylhydrazine (UDMH) as fuel and Nitrogen tetroxide (N2O4) as the oxidizer.

3. Cryogenic fuel: The third stage of the GSLV, also known as the GS3 or Cryogenic Upper Stage (CUS), uses cryogenic propellants. This includes Liquid Oxygen (LOX) as the oxidizer and Liquid Hydrogen (LH2) as the fuel. Cryogenic engines provide more thrust for every kilogram of propellant they burn compared to solid and earth-storable liquid propellant rocket stages.

Which type of fuel is used by GSLV in its operations?

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