PERSONAL AIR TRANSPORTATION SYSTEM

MODEL MA-1

SINGLE SEAT/ DUAL TANDEM SEAT,
VERTICAL TAKE OFF LANDING AIRCRAFT

PROPULSION:

Automotive gas/electric MA-1GE

Full electric MA-1E

SPECIFICATIONS:

Wing span ..............................20.00 ft

Length....................................30.00 ft

Height.......................................7 feet 2 inches

WING AREA

Fixed ............................68 sq ft

Rotary ..........................16 sq.ft


WEIGH (Gross Take off weight (GTW)

Single seat gas /electric .......1870 lbs

Single seat full electric ...........to be announced

PERFORMANCE

Predicted cruse speed between 110- 157 mph

Max suggested operating altitude under 12000 ft sea level

POWER PLANT

To be decided upon operators preference and requirements

COCKPIT: 

None pressurized, air conditioned heat/cool

Avionics : standard VFR + available IFR

SAFETY

Ballistic parachute/ shock absorbing airframe (standard)