Origin(s) | Italy (Fiat Aviazione) | ||||||||
|---|---|---|---|---|---|---|---|---|---|
Units Produced | 1 prototype | ||||||||
Engines and Powerplant | 1 × Fiat A.129 turboshaft engine (Power: approx. 770 kW / 1.030 horsepower) | ||||||||
Propulsion System | 6 ducted fans (ducted rotor system) Each fan mounted within a fixed frame | ||||||||
Control System | Altitude, Yaw, Roll controlled through the thrust direction and power of the fans | ||||||||
Maximum Takeoff Weight | approximately 2.500 kg | ||||||||
Maximum Speed | Approximately 210 km/h (theoretical) | ||||||||
Dimension(s) | Length: approx. 6.2 meters Rotor diameter (including ducts): approx. 4 meters Height: approx. 2.5 meters | ||||||||
First Flight(s) | Approximately 1 hour (based on test data estimate) | ||||||||
The Fiat 7002 was a helicopter prototype developed in Italy in the late 1950s. Designed for vertical take-off and landing (VTOL), it was intended primarily for heavy-lift transport.The aircraft aimed to offer a different approach to moving heavy loads, particularly in limited or hard-to-reach areas.

Fiat 7002 (Retro Transport)
The purpose of developing the Fiat 7002 was to provide a more efficient heavy-lift vehicle with vertical take-off and landing capability compared to standard helicopters. The project was initiated by Fiat Aviazione in the mid-1950s. The helicopter prototype was completed in 1958 and made its first free flight on January 26, 1961.
Fiat 7002 (Retro Transport)
The Fiat 7002 had a unique design compared to the helicopter standards of its time:

Fiat 7002 (Retro Transport)
The test flights of the Fiat 7002 demonstrated the feasibility of its "cold jet" propulsion system and its potential for cargo transport. The system was noted to have lower vibration and noise levels compared to conventional helicopters. However, it faced challenges with fuel efficiency. The turbogenerator system's inability to use jet fuel efficiently limited the aircraft's operational range and endurance. Additionally, technical complexities and economic conditions affected the project's progression. The Fiat 7002 remained a prototype and never entered commercial or military service.
The Fiat 7002 stands in aviation history as an example of experimental work on unusual propulsion systems and heavy-lift VTOL concepts. The "cold jet" rotor drive system was part of a broader search for alternatives to mechanical transmissions in helicopter design. Although it did not achieve commercial success, it is remembered as a demonstration of the effort to try different approaches in aviation engineering. The project provided data for the development of vertical take-off and landing technologies.
Aviastar. "Fiat 7002." aviastar.org. Accessed: 16 August 2025. https://www.aviastar.org/helicopters_eng/fiat-7002.php
Hargreaves-Miller, Richard. "Fiat 7002: The Flying Drinks Cabinet." Plane Historia. Accessed: 16 August 2025. https://planehistoria.com/fiat-7002/
Retro Transport. "Fiat 7002." YouTube. Accessed: 16 August 2025. https://www.youtube.com/watch?v=eShFefzdKLo
Whitemule. "Fiat 7002 Flying Caravan." El Poder de las Galaxias. Accessed: 16 August 2025. https://elpoderdelasgalaxias.wordpress.com/2019/06/02/fiat-7002-flying-caravan/
Origin(s) | Italy (Fiat Aviazione) | ||||||||
|---|---|---|---|---|---|---|---|---|---|
Units Produced | 1 prototype | ||||||||
Engines and Powerplant | 1 × Fiat A.129 turboshaft engine (Power: approx. 770 kW / 1.030 horsepower) | ||||||||
Propulsion System | 6 ducted fans (ducted rotor system) Each fan mounted within a fixed frame | ||||||||
Control System | Altitude, Yaw, Roll controlled through the thrust direction and power of the fans | ||||||||
Maximum Takeoff Weight | approximately 2.500 kg | ||||||||
Maximum Speed | Approximately 210 km/h (theoretical) | ||||||||
Dimension(s) | Length: approx. 6.2 meters Rotor diameter (including ducts): approx. 4 meters Height: approx. 2.5 meters | ||||||||
First Flight(s) | Approximately 1 hour (based on test data estimate) | ||||||||
Purpose of Development and History
Design and Technical Specifications
Operational Status and Fate
Significance and Legacy
This article was created with the support of artificial intelligence.