Martin Jetpack - Target 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.