Technical Information

Technical Information

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.

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