DRDO conducts successful ground test of full scale actively cooled long duration Scramjet Engine for Hypersonic Missile Programme

1. At a Glance

2. Why in the News

3. Background & Evolution

4. Core Static Facts

5. Multi-Dimensional Analysis

Scientific / Technological - Scramjet sustains supersonic combustion — fuel must ignite and burn in airflow moving faster than sound, the "lighting a match in a hurricane" problem. [S1][S2] - Active cooling uses fuel itself as coolant (regenerative) before injection — necessary because combustor walls face >2,000 °C heat fluxes for sustained burn. [S2] - Endothermic fuel absorbs heat by cracking into lighter hydrocarbons before combustion — boosts heat-sink capacity. [S2]

Geopolitical / Strategic - Joins US, Russia, China as nations with demonstrated long-duration scramjet capability. [S2] - Counters Chinese DF-ZF and Pakistani interest in hypersonics; strengthens India's credible minimum deterrent posture. [S3] - Hypersonic cruise missiles defeat current BMD systems (THAAD, S-400 class) via manoeuvrability + low-altitude flight at Mach 5+. [S3]

Economic / Industrial - Combustor and SCPT facility realised with Indian industry partners — reinforces Atmanirbhar Bharat in Defence and Defence Industrial Corridor (Hyderabad node). [S1] - Spin-off potential: hypersonic civil aviation, reusable space launch, high-temperature materials. [S2]

Administrative / Governance - Project under DRDO's Integrated Guided Missile Development Programme lineage; complements BrahMos-II (hypersonic) and Long Range Hypersonic Missile demonstrated Nov 2024. [S5]

6. Recent Developments (12–18 months)

7. Prelims Hooks

8. Mains Relevance

9. Related Topics to Study Next

10. Common Errors / Trap Areas

11. Sources