Scramjet
ISRO's Scramjet Engine Technology Demonstrator uses atmospheric oxygen to burn fuel, enabling extremely efficient hypersonic propulsion for future space missions.
Vehicle Specifications
Height
10.0 m
Diameter
0.5 m
Lift-off Mass
3 tonnes
Booster Stages
1 Stages
Payload (LEO)
0.0 kg
Payload (GTO)
0.0 kg
Modular Booster Stages
Stage 1
Solid BoosterProvides massive thrust at lift-off utilizing advanced HTPB solid propellants.
Launch Roster Performance
Mission Status
This launcher configuration is categorized under Active Launch Roster Fleet. It remains one of the fundamental benchmarks of ISRO's satellite deployment program.