Start of a micro-rocket with a satellite from a platform floating in the stratosphere.
Characteristics:
- Easy adaptation of the system to the weight of the satellite – modular design of balloons,
- Sheathing of the balloons,
- Manoeuvring thrusters enabling course corrections.
Competitive advantages:
- Multiply cheaper solution than conventional ones,
- Independence from current tycoons who have monopolized the market.
Application:
- Meterology, cartography and telemetry,
- Geolocation,
- ICT.
