TECHNICAL INFORMATION
Martin Jetpack Specifications
Download technical specification brochure
| Height |
5 ft |
| Width |
5.5 ft |
| Length |
5 ft |
| Structure | Carbon fibre composite |
| Empty weight | 250 lbs (excluding safety equipment) |
| Gross weight | 535 lbs |
| Useful (Pilot) Load | 280 lbs+ |
| Maximum thrust | 600 lbs+ |
| Fuel Capacity | 5 US gallons (as required by FAA Part 103,Ultralight Regulations) |
| Fuel burn | 10.0 gph |
| Engine | Martin Aircraft 2.0 L V4 2 stroke, rated at 200 hp (150 kw). Max 6000 rpm. |
| Electrical system | 12 V DC Battery, starter, 360 w alternator. |
| Rotor | Carbon / Kevlar composite diameter 1.7 ft |
| Max | 7058 rpm |
| Range | 31.5 miles (at max speed of 63 mph as required by FAA part 103). |
| Hover in ground effect | 8000 ft (estimated) |
| Hover above ground effect | 8000 ft (estimated) |
| Standard Equipment |
Flight and Engine displays Harness Ballistic Parachute Retractable undercarriage Energy absorbing undercarriage. |
| Classification | Meets the requirements of the FAA Part 103, Ultralight Regulations |
| Pilot License |
The Ultralight class does not require an FAA recognised pilots license. |
The Martin Jetpack is a unique aircraft and all owners are required to pass the Martin Aircraft Company approved training program before receipt of their aircraft.