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CE20 Cryogenic Engine

Posted 22 Jan 2025

Updated 24 Jan 2025

5 min read

Why in the News?

The Indian Space Research Organisation's CE20 cryogenic engine passed a critical sea-level test, a breakthrough in its propulsion technology.

More about the news

  • The sea-level test implemented a 'Nozzle Protection System' to manage issues like flow separation within the nozzle, which can cause vibrations, thermal problems, and potential damage.
  • ISRO has been working on the engine in view of its Gaganyaan mission, India's first manned spaceflight
  • Test Location: ISRO Propulsion Complex in Mahendragiri, Tamil Nadu.
    • The sea-level test introduced an innovative 'Nozzle Protection System' to address technical challenges in engine restart capability.
  • Earlier, HAL had also established the Integrated Cryogenic Engine Manufacturing Facility in Bengaluru, 2023. 

How does a cryogenic engine work?

  • The working principle: The thrust is produced by an internal combustion/pressure difference.
    • This follows Newton's Third law of motion- "Every action has an equal and an opposite reaction".
  • Uses: Cryogenic engines are used in space launch vehicles, in the last stage (or upper stage) of a rocket. 
    • A Cryogenic engine uses both cryogenic fuel and oxidizer, liquefied at a very low temperature. 
  • Fuel: The fuel and oxidizer used in a cryogenic engine are liquefied gases, stored at extremely low temperatures. 
    • Generally liquid hydrogen liquefied at -253° Celsius is used as fuel and liquid oxygen liquefied at -183° Celsius is used as oxidizer.

Note: Semi-cryogenic engine uses refined kerosene instead of liquid hydrogen which offers advantages of lighter weight and storage at normal temperature.

Advantages of cryogenic engine

  • Efficiency and Thrust: Compared to solid and earth-storable liquid propellant rocket stages, cryogenic propulsion offers superior thrust, with LOX+LH2 producing maximum energy and lightweight water vapor, resulting in higher performance.
  • Fuel Efficiency: Cryogenic engines use less fuel. ISRO's PSLV Vikas engine burns 3.4 kg/sec, while cryogenic engines need only 2 kg/sec for the same thrust. Their specific impulse reaches 450 seconds versus 260 seconds for solid propellants.
  • Eco-Friendly Technology: Hydrogen-oxygen combustion emits only steam, making cryogenic propulsion a clean, carbon-free solution.
  • Heavy Payloads & Space Missions: High efficiency makes cryogenic fuel ideal for heavy payloads and long missions like Gaganyaan and Chandrayaan.

Some of the challenges in Cryogenic engine technology

  • Complex technology: A very complex system compared to solid or liquid propellant stages due to its use of propellants at extremely low temperatures and the associated thermal and structural problems. 
  • High thermal gradient and thermal stresses: Problems such as cracks forming on the divergent outer shell, sudden stoppage of rotation, blockages in the channels, distortions in nozzles etc.
  • High Operational Pressures: The high operational pressures of thrust chamber coolant circuits and thrust related stresses typically require high strength super alloys for load reaction, ultimately a major engine weight driver.
  • Maintaining low temperature: The most significant thrust chamber challenge is balancing system performance with the thermal capability of coolant liners at deep throttle; low coolant flow operation.
  • High cost of development: Cryogenic Upper Stage (CUS) project in 1994 had budget of Rs 300 crore.

About CE20

  • Developed by: The Liquid Propulsion Systems Centre (LPSC), Valiamala, Kerala.
  • Output: It has been upgraded to produce a thrust level of 20 tonnes. Apart from that, it is capable of producing an enhanced thrust of 22 tonnes for the C32 stage in the future.
    • C32 is new and heavier cryogenic upper stage called C32, a variant of the C20 engine that will replace lesser capacity C25 stage.
  • Successful Mission: It has demonstrated its capability by successfully operating in six successive LVM3 missions, including the Chandrayaan-2, Chandrayaan-3, and two commercial OneWeb missions.
    • LVM3 (Geosynchronous Satellite Launch Vehicle Mk III) is three-staged vehicle, capable of lifting 4000kg payload.

Cryogenic Engine comparison with other engines

Characteristics

Cryogenic Engine

Jet Engine

Solid Propellant Engine 

Liquid Propellant Engine

Air Intake

No air intake is required.

Air intake is required.

Air intake is required as oxidizer.

Air intake is required as oxidizer.

Fuels

Generally super cooled Hydrogen and Oxygen.

(Jet A-1, kerosene),

Kerosene-gasoline mixture,

Aviation gasoline (avgas),

Bio-kerosene.

Fuels for composite propellants are generally metallic powders, with aluminum being the most common. 

Hydrazine, mono-methyl hydrazine (MMH), unsymmetrical dimethyl hydrazine (UDMH) etc.

Fuel temperature

The temperature of fuel must be

Very low.

Fuel storage does not require low temperature.

Fuel storage does not require low temperature.

Fuel storage does not require low temperature.

Efficient working

It runs efficiently when low temperature fuel transforms and mixes correctly and ignites.

It runs efficiently at supersonic speed that forcefully compresses air before combustion.

It runs efficiently when fuel is provided with sufficient oxidizer.

It runs efficiently when fuel is provided with sufficient oxidizer.

Purpose

Third stage/ last stage of rocket.

Used in the Airplanes etc.

Used as boosters in initial liftoff.

Act as main stage of rocket after booster separation.

Conclusion

The CE20 Cryogenic engine marks a significant milestone in ISRO's progress with cryogenic technology. Advancing further, ISRO could explore start fuel ampules like Tri-ethyl-aluminum and Tri-ethyl-boron to enhance ignition reliability and efficiency.

  • Tags :
  • ISRO
  • Semi-Cryogenic Engine
  • Cryogenic Engine
  • CE20
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