Burt Rutan is one of those designers for whom the sky has
never been the limit. He has a long history of reaching for seemingly
unattainable goals and winding up with designs that truly lead the way for other
builders. Since his first canard
machine, the stall proof Vari-Viggen of the mid-70s, Burt has dominated the
homebuilt aircraft market with airplanes such as the VariEze and Long EZ, the
Grizzly and, more recently, the innovative Beech Starship.
In 1975, however, Burt applied himself to the problems of
building a canard-controlled, centerline thrust twin, and the result was a Star
Wars design know as the Defiant. When
the airplane was introduced in prototype form, it caused quite a stir in the
general aviation market, especially considering that Rutan announced plans to
try to certify the Defiant for production.
The cost of certification, especially on such an
unconventional design, apparently scared off all the prospective investors, and
the prototype became little more than Burt’s personal transportation airplane.
To call this a shame is an understatement, as the defiant was a definite
step ahead in safety, performance and efficiency.
Unfortunately, it was perhaps a little too far ahead.
The Defiant might have been relegated to the file of those
ideas whose time hadn’t quite come but for the efforts of Fred Keller of
Anchorage, Alaska. Keller was a
veteran VariEze builder who had won Oshkosh with his remarkably slick airplane.
In mid-1981, Keller asked Rutan if he could build his own Defiant.
Knowing Keller’s reputation for quality workmanship, Rutan agreed
provided that Keller documented the building process so that Rutan could use the
information in the event he decided to offer the Defiant as a homebuilt or kit
airplane.
Keller finished his Defiant in 18 months, an unusually
short time for construction of an airplane, much less redesigning much of it
(with Rutan’s help and encouragement) and writing a full set of plans in the
process. Keller shot more than 750 photos of the buildup process and detailed
every step along the way. When he
was done, he had an airplane that was superior to the prototype in almost every
respect, plus he had one of the most comprehensive sets of plans ever assembled
for a homebuilt airplane.
Plans are available from Rutan Aircraft Factory in Mojave,
Calif., to build the Fred Keller version of the Defiant.
Currently, RAF is only offering plans ($490). The company may soon be
producing some components to ease the homebuilding job.
Make no mistake about it; constructing a Defiant will
probably be a major task, whether it’s your first airplane or your tenth.
Although the Defiant won’t necessarily be any more difficult to build,
it will be a large machine by homebuilt standards.
A builder will be doing nearly twice the work he’d put into a Long EZ.
There are obviously two engines to be mounted, total wing/canard area is
significantly greater and the fuselage is proportionately larger in order to
accommodate four people. Construction hour estimates may not mean much at this
stage, but one source at Rutan said he wouldn’t’ be surprised if total
buildup time ran 3000 hours.
At least when finished, a builder will have an unusual and
talented airplane. Like the canard
designs that preceded it, the Defiant reflects an overriding concern for the
health and safety of its passengers. Rutan pulled out all the stops when he
built the Defiant, designing an airplane that would effectively avoid all the
traps of twin-engine airplanes flown on one mill.
To better understand exactly what Rutan and Keller had
achieved in the Defiant, I went to Mojave and flew the prototype with RAF pilot
Mike Melvill. Once you walk up to the Defiant on the ramp, you know this is a
different breed of airplane. Like
all recent Rutan designs, the Defiant (technically designated the RAF-40 –
Rutan’s fortieth design) utilizes a canard on the nose for pitch control,
winglets and a retractable nosegear with fixed, slickly faired mains.
Typically, the Defiant realizes economies of design not possible on
normal twins. The RAF-40’s
airframe has a wetted area only 56 percent that of normal twins, and the
winglets offer 30 percent less induced drag by increasing the effective span.
Unlike even his single-engine designs, however, Rutan’s
Defiant mounts a pair of 160-hp O-320 Lycoming engines inline to eliminate any
possibility of asymmetric thrust, ala Cessna’s now out-of-production 337
Skymaster. Pilots who have flown
the Skymaster will tell you that it was, like the Defiant, a docile twin, but
that it suffered from other problems which virtually doomed it to failure from
the outset. Rutan’s ultimate
concern for safety has effectively sidestepped most of these problems so that
the defiant is a seemingly impossible ideal, an idiot-proof twin.
Climb aboard over the cabin walls and you find that the
cabin configuration is comfortable for the pilot and all three passengers.
The panel is spacious and wide, easily large enough to accept almost any
avionics you might install. (Radar would present a slight problem because the
wing is too narrow to accommodate the dish antenna.) Rutan’s prototype is
equipped with a full King package.
Engine start is conventional carburetted Lycoming.
Power controls are similar to those of twins with engines on the wings.
The left throttle controls the forward engine and has a small horn
pointing forward mounted to its left side, while the right manages power on the
rear, and accordingly has a horn pointing aft.
On Rutan’s airplane, you can, for all practical purposes, fly the
airplane as if it were a single and move both throttles together, whether on or
both engines are running.
That, in fact, is one of the great joys of the Defiant.
It’s an amazingly forgiving airplane in single-engine mode.
It wouldn’t be a particularly bright idea to initiate a single-engine
takeoff, however, especially at Mojave’s 3000-foot pressure altitude. (Cessna
found this to be a particularly vexing problem on the Skymaster, as some pilots
would blindly attempt to depart on the front engine alone after the rear engine
had idled out during taxi or runup. As
a result, the company developed the procedure of advancing the rear throttle
first on takeoff, then the front throttle.)
With both mills turning, normally, the Defiant responds
quickly to power application on takeoff, but don’t plan to use short runways.
The Defiant isn’t exactly a ground lover, but it’s not a STOL airplane
either.
Off the ground and stabilized at 100 knots with the nose
gear retracted, the Defiant climbs as if something big were chasing it. With
just Melvill and me aboard, I saw initial VSI readings of nearly 2000 fpm.
The spec for full gross (of 2900 pounds) at sea level is 1600, and I’d
guess the Defiant could easily achieve such a number.
Better still, the Defiant is capable of some tall
altitudes. Burt’s brother Dick
has had the airplane above 25,000 feet. Remember
the Defiant is carbureted and normally aspirated, not injected and turbocharged.
For our purposes, we tried altitudes from 6500 to 10,500
feet. At the higher altitude, I
tried some “stalls” and found them to be typically nonexistent.
Rutan has always been adamant that airplanes shouldn’t stall.
To that end, canard response is restricted so that you can’t get the
airplane into an attitude that will stall the wing.
Power-off, the Defiant will simply mush downhill under perfect control.
The right side stick is sensitive at high speeds but loads up rapidly as
angle of attack increases.
At 6500, the density altitude was probably about 8000 feet,
so we tried some cruise numbers with both throttles full forward, representative
of a maximum 75 percent effort.
Specifically, I saw an easy 175 knots True.
Pulled back to 65 percent, the number was more like 168 knots.
These are impressive numbers, but they’re even more significant when
you consider the low fuel consumption necessary to achieve them.
The O-320 Lycoming has always been an efficient engine, in addition to
being one of the most reliable general aviation powerplants on the market.
Specific fuel consumption (sfc) is low .44 pounds per horsepower. High
cruise costs only about 18 gph, while a 65 percent effort drains a mere 15 gph.
In more familiar terms, consider that you’re realizing more than 10
nmpg, even at high cruise, which is excellent efficiency for a twin-engine
aircraft.
In terms of cross-country cruise capability, the Defiant
should be a winner. With 110
gallons aboard and burn rate of only 15 gph at 65 percent, a pilot and three
passengers should be able to cover an easy 1000 nm between refueling stops.
But efficiency is only one of the Defiant’s talents.
Typical of all Rutan designs, the primary goal of the Defiant is safety,
and there’s no question that Burt has produced an unusually docile twin.
Mike Melvill let me discern exactly what the airplane could do under the
worst possible conditions: a single-engine go-around.
First, I set up for a 90-knot glide, gear down, with partial power on
both engines. Then, at 5500 feet
altitude, Melvill abruptly shut down the front engine and instructed me to cob
both throttles and lever the side stick straight back to the stop.
This could be insanity on any other twin, even one with
inline engines. It would violate
blue-line speed and result in a short zoom, followed by a rapid descent, and
out-of-control roll toward the dead engine and an abrupt landing in a vertical
attitude.
The Defiant’s
reaction was a 400-foot balloon in altitude, along with a bleed-off of airspeed
to around 55 knots.
Because there’s basically no stall in the Defiant, you
can hold full aft stick with relative impunity.
When I’d reached the top of the zoom, I began to milk the stick forward
to see how much of the altitude I could hold as I tried to stabilize airspeed at
the same 90 knots. To my amazement, the Defiant finished the exercise 300 feet
higher than it had entered.
The point is that all a pilot need do on a single-engine
go-around is push the throttles full forward and pull back on the stick to keep
the airplane flying. Remember, too,
that Melvill and I flew this exercise at 5500 feet, certainly not the best
altitude for single-engine go-arounds.
Like the Cessna Skymaster, the Rutan Defiant will perform a
little better on the rear engine, alone, than on the front engine, solo.
If you’re doing everything right, the rear engine should provide about
300 to 350 fpm, whereas the front engine will deliver more like 250 to 300 fpm.
(The propellers are pitched differently in order to compensate for the
difference, which is due to less fuselage drag with the front engine shut down
and not blowing confused air back across the rear prop.)
Admittedly, these numbers aren’t that much better than
conventional twins, but the difference is it takes little technique to achieve
them. The pilot of the Defiant can
do more things wrong when an engine fails and still come home with the airplane
– and, more importantly, himself – in one piece.
Back in the pattern, the Defiant exhibits some
characteristics that are atypical of other twins. If you’ve been flying a Long-EZ or VariEze, you’ll be
prepared for the Defiant’s glide ratio. Otherwise, it may come as something of
a shock. The airplane loves to fly, and even power off it gives up speed and
altitude grudgingly. Melvill
suggested that I hold 90 knots in the pattern.
My lack of recent experience with extremely slick Rutan designs almost
forced a go-around on the first attempt. Until
you’re used to the airplane’s power-off response, you’ll tend to
consistently overshoot the touchdown spot.
To further emphasize how clean the defiant is, Melvill had
me shoot several more approaches with the front engine shut down.
I might have assumed that the additional drag from an unfeathered,
fixed-pitch prop would have dramatically reduced gliding efficiency, but it
didn’t. The Defiant defiantly
glided as if both mills were still turning.
Because the Defiant’s glide is so flat, there’s an automatic tendency
to assume that you’re too low and thus add power, thereby only making things
worse.
The touchdown itself is ridiculously easy, provided you
keep the speed down. Come across
the fence 10 knots too fast and you’ll float into the next county.
The Defiant sets down nicely on the mains, after which you can lower the
nose gently to earth.
Like all of Rutan’s designs, the Defiant is a cut above
the average. It’s an unusual
machine that’s sure to be attractive to the pilot who wants something a little
different – make that a lot different. Not
everyone will be able to afford the time necessary to build a Defiant, however.
The cost will be more than money.
For those who can justify the effort and expense, the
Defiant is a Tomorrowland design here today.
It offers truly 21st century performance and safety.
Rutan Defiant:
Specifications:
Homebuilt price: $20,000 to $40,000
Engine(s) make/model: Lycoming O-320 (2)
Horsepower @ rpm @ altitude:
160 @ SL
Horsepower at takeoff: 160
TOB hours: 2000
Fuel type: 100 Octane
Landing gear type: Partial retractable
Max Ramp weight (lbs): 2950
Gross Weight (lbs) 2950
Max Landing weight (lbs): 2950
Empty weight (std) (lbs): 1600
Equipped weight (as tested) (lbs): 1680
Useful load (std)(lbs): 1350
Payload (full std fuel) (lbs): 580
Fuel capacity (std) (gals): 115
Wingspan: 31ft 5in
Wing area (sq.ft.): 22.2
Wing loading (lbs/sq.ft): 22.2
Power loading (lbs/hp): 9.2
Seating capacity: 4
Cabin doors: 0
Cabin width (in).: 46
Baggage capacity (cu/ft): 41
PERFORMANCE:
Cruise speed (kts):
75% pwr: 8,000ft @ 184 best power
55% pwr: 9,000ft @ 168 best power
Max range (reserve/no reserve)(nm):
55% pwr: 1044
Fuel consumption (gph):
75% pwr: 17.8
55% pwr: 13.9
Estimated endurance (55% pwr) (hrs): 8
Stall speed (gear down) (kts): 64
Best rate of climb (fpm): 1900
Single-engine rate of climb (fpm): 310 (rear)
Service ceiling (ft): 28,000+
Single-engine service ceiling (ft):6500
Aircraft Comparison
Chart:
| Aircraft |
Rutan
Defiant |
Piper
Seneca III |
Beech
B-55 |
Cessna
Crusader |
| Price: |
$30,000 |
$200,000 |
$350,000 |
$330,000 |
| Cruise (kts): |
184 |
192 |
182 |
182 |
| Stall (kts) |
64 |
61 |
68 |
61 |
| Range (nm): |
1040 |
765 |
822 |
850 |
| Fuel (ghp): |
18 |
24 |
29 |
28 |
| Climb (fpm): |
1900 |
1340 |
1670 |
1480 |
| Serv. Ceiling (ft): |
28,000 |
25,000 |
19,700 |
25,000 |
| Takeoff over 50' obs: |
N/A |
1210 |
1225 |
1750 |
| Landing over 50' obs: |
N/A |
2160 |
1370 |
1450 |
| Useful load (lb): |
1270 |
1900 |
2000 |
1695 |
| Power loading (lbs/hp): |
9.2 |
10.8 |
N/A |
9.9 |
| Horsepower: |
320 |
440 |
520 |
520 |
| Prop type: |
Fixed |
C/S |
C/S |
C/S |
| Landing gear type: |
Partly Retract |
Retract |
Retract |
Retract |
| Fuel Capacity (gals): |
115 |
123 |
142 |
150 |
| Seat Capacity: |
4 |
4 |
6 |
6 |