Technical

Martin Jetpack Layout

The Target Technical Specifications for our First Production Model are detailed below

General Characteristics:

Type Class one microlight
Crew Single pilot
Height (m) 2.20
Width (m) 2.14
Depth (m) 1.75
(pilot module)
Aircraft empty weight 200kg (manned)
Max aircraft take-off weight 320kg
Payload at full fuel (Pilot + Equip weight) 120kg
Engine 200hp, 100hr TBO, low vibration
Fuel capacity 45 litre

 

    

Performance:

Range 30km-50km
Endurance (flight time) 30 minutes + Reserves
Maximum airspeed 40kts (74km/h)
Cruise speed 30kts (56km/h)
Ceiling 3,000 ft AMSL
Recommended cruise height 500ft and above per aviation authority regulations
Take-off wind limit 15kts gusting +/- 5kts (28km/h +/- 9km/h)

 

    

Composite Airframe Specifications

Ducts Carbon fibre, aramid fibre, honeycomb core, epoxy resin
Fans Epoxy prepreg carbon fibre, aramid fibre, foam core
Main Beam High modulus carbon fibre, foam core
Spine Epoxy prepreg carbon fibre
Fuel Tank Carbon fibre, Kevlar, fuel resistant epoxy resin
Undercarriage Carbon fibre, epoxy resin, aluminium alloy
Engine Heads High precision CNC machined aluminium, twin spark plugs per cylinder.
Airboxes Fabricated from aluminium

 

    

Other Specifications:

Fuel and oil Runs on automotive gasoline and 2 stroke oil
Starting Internal starter
Computer aided stability "Fly by wire", no-pilot-control-input produces a zero air-speed hover
Aircraft operating rules Daylight and visual flight only (Night vision operations possible)
Ballistic Parachute Ultra low level opening Ballistic chute integrated into the FCS and EMS
Pilot protection Protective pilot module and structural protection

 

Downloadable PDF