Recently, DRDO successfully conducted a ground test of an Active Cooled Scramjet Subscale Combustor for over 1,000 seconds, marking a major step toward developing indigenous hypersonic cruise missiles.
About Hypersonic Technology
- Hypersonic vehicles travel at speeds greater than Mach 5, meaning they exceed 6,100 km/h, enabling rapid global reach and tactical superiority.
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About Mach
- The Mach is a dimensionless quantity representing the ratio of an object’s speed to the speed of sound in the surrounding medium.
- It is used as a unit to measure high-speed motion, where 1 Mach equals approximately 1,235 km/h at sea level.
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- Scramjet Engines: Supersonic Combustion Ramjet (Scramjet) engines enable sustained hypersonic flight by using atmospheric air, making the system lighter and more efficient than traditional rockets.
- The Active Cooled Combustor technology uses advanced cooling techniques to endure extreme thermal loads during hypersonic flight, ensuring longer operational durations.
- Global Race in Hypersonic Systems: Nations like China, Russia, and the United States are actively developing hypersonic weapons, highlighting the strategic urgency for India to advance its own capabilities.
Significance of DRDO Achievement for India
- Breakthrough in Endurance Testing: DRDO’s successful 1,000-second ground test, a significant leap from previous 120-second tests, validates the endurance and reliability of hypersonic combustion systems for real-world applications.
- Foundation: The achievement provides a critical technological foundation for the future development of India’s indigenous hypersonic cruise missiles, enhancing both strategic deterrence and precision strike abilities.
Self-Reliance: This milestone strengthens India’s Atmanirbhar Bharat initiative by reducing dependency on foreign technologies in crucial defence sectors and advancing high-end indigenous innovation.
- Strategic Relevance: By progressing towards operational hypersonic systems, India narrows the technology gap with global powers and improves its second-strike nuclear deterrence capabilities, crucial for maintaining strategic stability.
Subsonic, Supersonic and Hypersonic Cruise Missile
Aspect |
Subsonic Cruise Missiles |
Supersonic Cruise Missiles |
Hypersonic Cruise Missiles |
Speed |
Travel below the speed of sound (less than Mach 1( Around 1,225 km/h). |
Travel faster than sound, typically between Mach 1 to Mach 3 (1,225 to 3,675 km/h). |
Travel at speeds greater than Mach 5 (over 6,100 km/h). |
Propulsion |
Use turbofan or turbojet engines optimized for low-speed efficiency. |
Employ ramjet or scramjet engines for sustained high-speed flight. |
Powered mainly by scramjet engines with advanced air-breathing technology. |
Maneuverability |
High maneuverability but relatively easier to detect and intercept. |
Moderate maneuverability and reduced interception time. |
Extremely high maneuverability, making interception highly difficult. |
Examples |
Tomahawk (USA), Nirbhay (India). |
BrahMos (India-Russia), P-800 Oniks (Russia). |
Avangard (Russia), Dark Eagle (U.S) |
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