HYPERSONIC MISSILE
- The missile is a hypersonic cruise weapon capable of travelling at speeds greater than Mach 5, or approximately 6,100 km per hour, for sustained durations.
- This capability has been made possible through an advanced supersonic air-breathing propulsion system that employs indigenously developed liquid hydrocarbon endothermic fuel, high-temperature Thermal Barrier Coating (TBC), and sophisticated manufacturing technologies.
- It is equipped with an advanced actively cooled scramjet combustor featuring a novel flame-stabilisation mechanism that enables a continuous combustion process even when air flows through the combustor at speeds exceeding 1.5 km per second.
- The Thermal Barrier Coating (TBC) has been jointly developed by the Defence Research and Development Laboratory and facilities under the Department of Science and Technology.
- This specialised coating is engineered to endure the extremely high temperatures generated during hypersonic flight. The newly developed ceramic-based TBC possesses superior thermal resistance and can function at temperatures exceeding the melting point of steel.
- Hypersonic missiles are advanced weapon systems capable of travelling at speeds greater than Mach 5, which means at least five times faster than the speed of sound.
- Depending on atmospheric conditions, this translates to speeds exceeding nearly 6,000 km per hour.
- Their combination of extremely high speed, manoeuvrability, and lower flight trajectory makes them difficult to detect, track, and intercept compared to conventional ballistic missiles.
- These weapons are considered a major advancement in modern military technology because they can rapidly strike targets while reducing the reaction time available to defence systems.
- Hypersonic Glide Vehicles are first launched into the atmosphere using a rocket booster. After reaching a certain altitude, the glide vehicle separates from the rocket and glides toward its target at hypersonic speeds
- Ballistic missiles operate on the principle of projectile motion to deliver warheads to designated targets. They remain powered only during the initial phase of flight, after which they travel largely under the influence of gravity and aerodynamic forces.
- These missiles are generally classified according to their operational range and may be equipped with either conventional or nuclear warheads.
- A major feature that distinguishes hypersonic cruise missiles from ballistic missiles is their manoeuvrability.
- Unlike ballistic missiles, which follow a predictable ballistic path, hypersonic missiles can alter their trajectory during flight and navigate dynamically toward their intended targets.
- Cruise missiles typically travel at relatively low altitudes close to the Earth’s surface, whereas ballistic missiles move along a high-altitude parabolic trajectory.
- Because ballistic missiles follow a more predictable flight path, they are comparatively easier to detect and track.
- In contrast, the high manoeuvrability and low-altitude flight profile of cruise missiles make them more challenging for air defence systems to intercept
- Air-breathing propulsion technology has the potential to revolutionise launch vehicle design.
- According to Indian Space Research Organisation, various global space agencies are actively developing three major categories of air-breathing engines: Ramjet, Scramjet, and Dual-Mode Ramjet (DMRJ).
- In ramjet propulsion systems, the engine relies on the vehicle’s forward speed to compress incoming air for combustion, eliminating the need for a rotating compressor.
- Fuel is injected into the combustion chamber, where it combines with the compressed hot air and ignites. Since ramjets cannot generate thrust at low speeds, they require external assistance, such as rocket boosters, to accelerate the vehicle to operational speed.
- ISRO notes that ramjet engines perform most effectively at supersonic velocities of around Mach 3 and can function up to approximately Mach 6.
- However, their efficiency declines once the vehicle enters the hypersonic speed regime.
- A Supersonic Combustion Ramjet, commonly known as a Scramjet, is a more advanced form of ramjet engine designed for efficient operation at hypersonic speeds.
- Unlike conventional ramjets, scramjets enable combustion while the airflow inside the engine remains supersonic.
- In this system, air enters through the front intake, fuel combusts in the central chamber, and high-speed exhaust gases exit from the rear to generate thrust.
- A Dual-Mode Ramjet (DMRJ) combines the operational features of both ramjet and scramjet technologies.
- Within the Mach 4 to Mach 8 speed range, the engine transitions from ramjet mode to scramjet mode, allowing it to function efficiently under both subsonic and supersonic combustion conditions
- On May 7, the Defence Research and Development Organisation in collaboration with the Indian Air Force successfully conducted the maiden flight test of the TARA system, a technology designed to convert unguided munitions into guided weapons.
- The TARA glide weapon system mainly functions as a modular attachment that can be integrated with a standard unguided warhead. Once fitted, it enables the weapon to glide across extended distances and engage targets with greater accuracy.
- The system is understood to employ a combination of inertial navigation technology and satellite-based guidance for directing the missile toward its designated target.
- Instead of depending on a rocket propulsion mechanism, the TARA system operates through a glide-based approach. This design makes the weapon comparatively lightweight and economical while also enhancing its operational range.
- Through this technology, conventional unguided or gravity bombs can be upgraded into precision-guided smart munitions with minimal modification. As a result, the need for developing completely new missile platforms can be significantly reduced
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For Prelims: Tactical Advanced Range Augmentation (TARA) system, Ballistic missiles, Hypersonic missiles
For Mains: GS III - Science and technology
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Previous Year Questions
1.Consider the following statements: (UPSC CSE, 2023)
1. Ballistic missiles are jet-propelled at subsonic speeds throughout their flights, while cruise missiles are rocket-powered only in the initial phase of flight. 2. Agni-V is a medium-range supersonic cruise missile, while BrahMos is a solid-fuelled intercontinental ballistic missile. Which of the statements given above is/are correct? (a) 1 only (b) 2 only (c) Both 1 and 2 (d) Neither 1 nor 2 |
