SFDR Ramjet Technology Tested by DRDO
Why in the news
DRDO successfully demonstrated SFDR propulsion from the Integrated Test Range at Chandipur.
Key facts
- SFDR is an air-breathing system: air supplies the oxygen, solid fuel burns in a regulated way.
- Unlike a conventional rocket, it keeps thrust going at supersonic speed and holds energy for the terminal phase.
- No onboard oxidiser means more fuel space and longer range.
- Continuous thrust allows sharp evasive turns, making interception hard.
| Stage | What happens |
|---|---|
| 1. Acceleration | Nozzle-less booster lifts the missile to the required Mach number. |
| 2. Ramjet takeover | Forward motion compresses incoming air; no rotating compressors. |
| 3. Combustion | Solid fuel burns steadily under an indigenous fuel flow control system. |
| 4. Thrust | Steady push keeps the missile fast and manoeuvrable until impact. |
Significance
- Suited to BVRAAMs: long-range engagement, high kill probability, first-strike edge.
- Cuts reliance on foreign propulsion, supporting Aatmanirbhar Bharat.
Exam angle
- Developer: DRDO; site: Chandipur.
- Engine type: air-breathing, solid fuel, nozzle-less booster.