PROJECT AURORA

NTUA's First Solid Propellant Sounding Rocket

3km Target Apogee
1.3kg Payload Mass
2024 Launch Year

Our Mission

Aurora is a student-driven project dedicated to designing, manufacturing, and launching sounding rockets. Our team brings together expertise from multiple engineering disciplines to create advanced systems that push the boundaries of rocketry.

The project serves as a platform for exploration and innovation, enabling the development of rockets capable of achieving greater altitudes and improved performance.

Technical Specs

Aurora at a Glance

Solid Propellant

Advanced solid propellant motor designed for reliable, high-thrust performance

Target Apogee

Designed to reach 3km altitude with active airbrakes for precision control

Airbrakes System

Active control system for precise apogee targeting and trajectory management

Dual Deployment

Two-stage parachute system ensuring safe recovery after flight

1.3kg Payload

Payload compartment for scientific experiments

Advanced Avionics

Custom PCBs with telemetry, navigation, and flight control systems

Engineering

Key Subsystems

Cutting-edge technology across every component

Structural Design

Aerostructures

Advanced composite and metallic materials. FEA simulations ensure structural integrity under extreme flight conditions.

  • 3D CAD Design
  • FEA Analysis
  • Composite Manufacturing
Airbrakes System

Active Airbrakes

Precision control system for apogee targeting. Real-time deployment based on flight computer data.

  • Automatic Control
  • Real-time Adjustment
  • Precision Targeting
Recovery System

Recovery System

Dual deployment parachute system with drogue and main chutes for safe landing.

  • Dual Deployment
  • Ejection Mechanisms
  • Safe Landing
Avionics System

Flight Avionics

Custom PCBs with embedded systems for telemetry, navigation, and sensor integration.

  • Custom PCBs
  • Telemetry System
  • Sensor Integration
Payload System

Scientific Payload

4kg deployable payload for atmospheric research and microplastics detection experiments.

  • Deployable Design
  • Research Instruments
  • Data Collection
Aerodynamics

Aerodynamics

CFD simulations and wind tunnel testing for optimal nose cone and fin geometry.

  • CFD Analysis
  • Wind Tunnel Tests
  • Optimized Geometry
Development

Build Gallery

From design to manufacturing

Interested in Project Aurora?

Follow our progress on social media or reach out to learn more about our work