Our Projects

Explore our ongoing research and development projects in rocketry and aerospace technology.

LKD-12(2C)1A-1

Active

A liquid bipropellant rocket engine designed to deliver 1000N of thrust using Jet A-1 fuel.

Key Specifications

  • Chamber Pressure: 25 bar

  • Chamber Temperature: 3260 K

  • Isp: 274.2 s

  • Mass Flow Rate: 0.44 kg/s

  • O/F Ratio: 2:1

Milestones

Design Phase

Completed initial design and calculations

Component Testing

Individual component validation

Integration

System assembly and preliminary testing

Hot Fire Testing

Full engine test campaign

Technical Details
Development Updates

More Projects Coming Soon

Stay tuned for updates on our upcoming projects and research initiatives.