From light shows to space flights

Technical characteristics of RAD for launching space rockets (concept)

- Number of motors/rotors: 8; 4 pairs of coaxial electric motors with propellers

- Top rotor diameter: 7 meters

- Bottom rotor diameter: 5 meters

- Power: 300 hp on the engine, 2400 hp to a speed dial drone (RAD)

- Payload: 6000 kg on RAD

- Device weight with battery: 3000 kg

- Maximum takeoff weight: 9000 kg

- Maximum vertical speed with payload: 500 km / h

- Maximum height with load: 5000 m

- Flight time with payload: 4 minutes

- Flight time before launching a rocket at an altitude of 5000 meters: ~ 90 seconds

Tech for Good