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While
this is a good overview of Skycar use, you might want to also go to Skycar main web
site www.moller.com
This overview had been proceeded by an executive summary
which has not been updated since 1998 and has no graphics.
The dream is a reality
People have dreamed about a small air
vehicle for years, but until now a practical one has not been
available. The Moller 400 Skycar is the first such vehicle,
an automobile-sized vertical takeoff and landing (VTOL)
aircraft for a maximum of 4 passengers.
The M400 Skycar is designed to cruise at maximum speeds of 350 mph at maximum
altitude of 30,000 ft. Initially the FAA laws and fuel economy will
limit cruising speeds to 285 mph at altitudes below 10,000 ft.
It can fly a maximum of 900 miles without needing to be refueled.
Quick, automatic fine adjustment and
maneuvering are executed through computer control to produce
a smooth flight. With advanced avionics, the Skycar will be
simple to fly, and will eventually be capable of complete
electronic piloting.
Cabin pressurization or oxygen will be
provided to make use of the faster speeds available at high altitudes.
Motorized landing gear wheels will provide
taxiing to parking or takeoff areas.
However, the
prototype Skycar is
not designed to be used on roads.
The Skycar is unique
The M400 Skycar is classified
by the FAA as a
"powered lift" vehicle. The- 4 pairs of rotary engines
with ducted fans produce 1200 hp which provide 2800 lb of
thrust.
The four M400 engine nacelles each
provide 700 lbs of vertical lift and together can lift the vehicle more than a
mile in 60 seconds.
Moveable vanes mounted behind the
engines direct thrust to control the direction of flight -
vertical, horizontal, banking, turns, etc. No ailerons,
flaps, or other external control surfaces are necessary. The
speed of each engine and the position of the vanes are the
only control variables.
The vehicle's shape provides aerodynamic
lift and good fuel economy when cruising. Only 4 of the 8
engines, operating at less than 2/3 capacity, would be needed
to maintain cruising speed at altitudes below 10,000 ft.
The M400 uses gasoline.
Depending on
altitude and cruise speed, the Skycar can be expected to get
18 to 22 mpg. Each takeoff requires approximately 1/10
gallon of gas. The M400's rotary engines will soon be
capable of using other fuels, such as methanol, ethanol, jet
fuel, diesel, liquid natural gas, and hydrogen.
The satellite-based Global Positioning
System with emergency ground-based radio navigation
will provide instant,
accurate navigation. An obstacle-avoidance radar looking
forward and down can be added for safety.
Communications with a Skycar ground
controller will be facilitated by automatic position
reporting through efficient radio and satellite transmission.
Ground-to-Skycar and Skycar-to-Skycar communications will
also be available from commercial cellular telephone and/or packet
communication.
A practical Skycar can now be built
Moller's patented improvements to the
rotary engine provides sufficient lift per pound of engine
weight to permit making a practical 4-passenger Skycar. Twenty five years ago, a similar vehicle design was tried by the Navy,
the X22A. Until the powerful, low cost and lightweight
Moller engine was available, a practical ducted fan air vehicle could not be built.

Ducted Fans Were Too Large, Heavy, and
Expensive 25 Years Ago
Avionics (computers, controls,
radio communications, etc.) have evolved to the point of
being light enough, cheap enough, and capable enough to
control flight with multiple engines. Avionics also provides obstacle
avoidance, path planning and navigation.
The development of composite
materials are now light-weight, strong, and avaiable in optimum
aerodynamic shapes at reasonable cost. Composite airframes
have been used since the Learjet in 1981.
Designed
to be safe
The M400 Skycar will be able to take off
and land vertically with one engine inoperable, and can fly and land
safely with several engines inoperable. It has no component which can
fail catastrophically, such as a helicopter's main rotor or small
airplane's single engine.
Engines, computers, radios, radars,
communications, and navigation systems all have emergency functionality, so
the failure of a single part will not be flight-critical.
New, lightweight, inexpensive
radars and quick maneuverability will allow the Skycar
to operate safely close to buildings, power lines, trees,
etc., and avoid aircraft. Other
aircraft will never have the maneuverability required
for safe electronic piloting in close quarters or turbulent
conditions.
A phased array radar capable of
detecting wires and birds was demonstrated in the late
80s which weighed only 52 lbs. The manufacturer
estimated that the production weight would be less than 30 pounds, and cost
approximately $10,000.
Skycars are more like high-tech
bats
than conventional aircraft. Both can land almost anywhere, quickly
change direction, fly without crashing into other members of
the flock, are not dependent on ground control, and are able to sense range
to other objects.
The Skycar design permits very fast
changes in speed and/or direction. The thrust can be changed
by 10% in velocity or direction in 1/10 of a second.
The M400 Skycar will be much less
dangerous for bystanders than a helicopter or small airplane. The whirling fan blades are contained in
housings lined with kevlar. Screens provide protection to passengers
and vehicle even if
the blades should self-destruct.
A computerized vehicle condition
management system will constantly monitor engine and other
functions and stress points on the Skycar, and warn of
maintenance needed or impending failure. A trip can be
aborted safely if necessary, and another Skycar dispatched to pick up passengers.
Comparison of Aircraft
|
| |
Skycar
|
Helicopter
|
Airplane
|
| Capability |
Moller
|
McDonnell
|
Single
Engine
|
| |
M400
|
Douglas
520N
|
TBM 700
|
| Passengers |
4
|
4 to 5
|
4 to 7
|
| Cruise speed |
350 mph
|
155
mph
|
293
mph
|
| Top speed |
390 mph
|
175
mph
|
345
mph
|
| Rate of climb |
7,150 fpm
|
1,850
fpm
|
2,300
fpm
|
| Payload with max fuel |
740 lbs
|
1,403
lbs
|
615
lbs
|
| Max. range @ payload |
900 mi
|
250 mi
|
1,800
mi
|
| Fuel consumption |
18-22 mpg
|
4 mpg
|
7 mpg
|
| Operational ceiling |
30,000 ft
|
14,000
ft
|
30,000
ft
|
| Gross weight |
2,400 lbs
|
3,350
lbs
|
6,250
lbs
|
| Dimensions -
L*W*H |
18'x9'x6'
|
28'x27'x9'
|
34'x40'x13'
|
| Engine power |
960 hp
|
450 hp
|
700 hp
|
| Takeoff and landing area |
35 ft diameter
|
75 ft
diameter
|
3500
ft x100 ft
|
| Noise at 500 feet |
65 dba
|
75 dba
|
70 dba
|
| Price new - 1998 $ |
$996,000
|
$850,000
|
$1,800,000
|
The Skycar can land
very quickly on almost any stable flat surface such as a
parking lot or field. The Skycar can also make an
emergency landing at an airport.
Early in its development when a human
pilot is required, the Skycar will be an extraordinarily safe
small aircraft.
The Skycar will be even safer when full
electronic piloting is added. When added, pilots will not be
required to make split-second decisions in difficult
situations. The combination of electronic pilot backed up by
a ground controller will virtually eliminate errors made
under conditions of fatigue, drunkenness, poor visibility, or
distraction.
In the highly unlikely event that
several engines fail, two ballistic parachutes on the
airframe will prevent a fatal crash. The Skycar's
aerodynamic body provides a 9 to 1 glide slope for making an
emergency landing at an airport or open area with parachutes.
If a parachute landing is needed over
water the Skycar will float, enabling passengers to debark
with life preservers. The proposed design should be able to
land and take off from water.
The Skycar will also be safer than an
automobile because it is not limited to a single dimension
for maneuvering. It has no road edges, guard rails or
slippery roads to avoid, no dangerous traffic congestion, and
no mechanical failure or human error to contend with.
With the electronic pilot, the Skycar
accident rate should be lower than for other aircraft. The Skycar
will react quickly, have more maneuverability, will follow
safe electronic flight rules, will have radar observability
for at least 5 miles ahead, and will have communication with
other vehicles as well as with the ground controller.
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