LATEST NEWS :
Mentorship Program For UPSC and UPPCS separate Batch in English & Hindi . Limited seats available . For more details kindly give us a call on 7388114444 , 7355556256.
asdas
Print Friendly and PDF

Hypersonic cruise missile

17.07.2025

Hypersonic cruise missile

 

Context

 

India recently tested its first hypersonic cruise missile, ETLD HCM, marking a major leap in homegrown defense technology and strategic deterrence capabilities.

 

About the News :

  • India tested the ETLD HCM, a hypersonic missile under Project Vishnu, developed by DRDO.
  • The test confirms India’s entry into the elite hypersonic missile group (with US, China, Russia).
  • ETLD HCM uses a scramjet engine, achieving Mach 8 speed with 1,500 km range.
  • PIB confirmed the test; it was also reported by Indian Express and Economic Times.
     

 

Key Characteristics of Test: 

  • Speed: Achieves Mach 8 (eight times the speed of sound), ensuring high strike velocity.
  • Engine: Uses scramjet, which draws oxygen from air, improving speed and fuel efficiency.
  • Range: Covers up to 1,500 km, suitable for both tactical and strategic operations.
  • Payload: Carries nuclear or conventional warheads, up to 2,000 kg.
  • Launch Platforms: Can be launched from land, air, or sea, enhancing deployment flexibility.
  • Stealth: Very hard to intercept by even advanced air defense systems like S-500.
     

Difference between Cruise and Ballistic Missile

Point of Difference

Cruise Missiles

Ballistic Missiles

1. Flight Path

Flies at low altitude, terrain-hugging, pre-programmed route

Follows a high, parabolic arc; exits and reenters the atmosphere

Examples

BrahMos, Tomahawk, Nirbhay

Agni V, Prithvi-II, Trident II D5

2. Guidance

Fully guided throughout flight using GPS, terrain mapping, etc.

Guided only during boost phase; unguided during midcourse and terminal phases

Examples

JASSM, Storm Shadow/SCALP

Minuteman III, DF-26, Iskander-M

3. Speed

Subsonic or supersonic (e.g., BrahMos is supersonic)

Supersonic to hypersonic (e.g., ICBMs reach over 20,000 km/h)

Examples

Kalibr, AGM-86 ALCM

Hwasong-15, Agni III

4. Range

Medium to long-range, typically 500–2,500 km

Wide range: from <1,000 km (SRBM) to >5,500 km (ICBM)

Examples

Nirbhay (~1,000 km)

Agni V (>5,000 km), DF-5 (ICBM)

5. Detectability

Difficult to detect due to low altitude and small radar cross-section

Easily detected during boost due to heat and altitude

Examples

BrahMos avoids radar detection

Agni II visible on radar during launch

6. Tactical Use

Used for precise strikes on military or strategic targets

Used for strategic, long-range attacks (often nuclear delivery)

Examples

SCALP used for pinpoint strikes

Trident II for nuclear deterrence

 

Types of Jet Engines

Type

Key Features

Turbojet

– One of the earliest jet engine designs.

– Air is compressed using a turbine and fuel is burned to generate high-speed exhaust.

– The fast exhaust gases create forward thrust.

Turboprop

– A gas turbine drives a propeller to generate motion.

– Commonly used in small aircraft flying at low speed and altitude.

– Thrust mainly comes from the spinning propeller rather than exhaust gases.

Turbofan

– Widely used in modern commercial airplanes.

– Combines features of turbojet and turboprop engines.

– Some of the air bypasses the combustion area, helping create extra thrust with less fuel use.

Ramjet

– An engine that compresses air by using the aircraft’s high-speed forward motion.

– Lacks any rotating parts like turbines.

– Works effectively only at supersonic speeds.

Scramjet

– A faster version of the ramjet, designed for hypersonic speeds.

– Air enters and burns at supersonic velocity inside the engine.

– Efficient above Mach 5, mainly in high-speed aerospace applications.

Pulsejet

– A simple engine with no moving parts.

– Generates thrust through repeated combustion pulses.

– Less efficient and mostly used in model aircraft or experimental rockets.

 

Challenges

  • High-cost R&D: Hypersonic systems need advanced infrastructure, increasing cost. E.g., Scramjet test beds are rare.
     
  • Thermal stress: Sustaining 2,000°C heat is difficult. E.g., Needs special coatings and materials.
     
  • Guidance complexity: Requires precise navigation at high speed. E.g., Small errors cause large deviation.
     
  • Production delay: Large-scale rollout may take years. E.g., Not operational before 2030.
     

 

Way Forward

  • Strengthen R&D: Increase funding for indigenous hypersonic tech. E.g., Expand DRDO’s Aeronautics facilities.
     
  • International collaboration: Learn from friendly nations' expertise. E.g., Joint research with France or Israel.
     
  • Private sector role: Involve Indian industries for faster production. E.g., Like L&T in missile production.
     
  • Test integration: Conduct field tests with tri-forces. E.g., From submarines, jets, and mobile platforms.
     

 

Conclusion

The ETLD HCM positions India as a global hypersonic power, boosting national security and deterrence. With continued investment, it can transform India’s strategic and technological defense capabilities.

Get a Callback