Top Speed @ 100% Power (TIO-360/210 HP, @ Sea Level, IAS) 272 mph
Max Range @ 55% Power (TIO-360/210 HP, 10,000 ft., TAS) 247 mph
Cruise @ 75% Power (TIO-360/210 HP, 10,000 ft., TAS) 274 mph
Range @ 75%-55% Power (TIO-360/210 HP, 10K ft., TAS) 1459 - 1993 sm
Fuel Consumption @ 75%-55% Power (TIO-360/210 HP, 10K ft., TAS) 14.4 - 8.7 gph
Miles per gal. @ 75%-55% Power (TIO-360/210 HP, 10K ft., TAS) 20.84 - 28.47 mpg
Cruise @ 75% Power (TIO-360/210 HP, 25,000 ft., TAS) 323 mph
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Top Speed @ 100% Power (3.3 ltr. Subaru/260 HP, @ Sea Level, IAS) 292 mph
Max Range @ 55% Power (3.3 ltr. Subaru/260 HP, 10,000 ft., TAS) 265 mph
Cruise @ 75% Power (3.3 ltr. Subaru/260 HP, 10,000 ft., TAS) 294 mph
Range @ 75%-55% Pwr (3.3 ltr. Subaru/260 HP, 10K ft, TAS) 1455 - 2047 sm
Fuel Consumption @ 75%-55% Power ( " " ) 14.1 - 9.1 gph
Miles per gal. @ 75%-55% Power ( " " ) 20.78 - 29.24 mpg
Cruise @ 75% Power (3.3 ltr. Subaru/260 HP, 25,000 ft., TAS) 347 mph
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Top Speed @ 100% Power (3.3 ltr. turbo'd Subaru/350 HP,@ Sea Level,IAS) 323 mph
Max Range @ 55% Power (3.3 ltr. turbo'd Subaru/350 HP, 10,000 ft., TAS) 292 mph
Cruise @ 75% Power (3.3 ltr. turbo'd Subaru/350 HP, 10,000 ft., TAS) 324 mph
Range @ 75%-55% Pwr (3.3 ltr. turbo'd Subaru/350 HP, 10K ft, TAS) 1193 - 1679 sm
Fuel Consumption @ 75%-55% Power ( " " ) 19.0 - 12.2 gph
Miles per gal. @ 75%-55% Power ( " " ) 17.05 - 23.98 mpg
Cruise @ 75% Power (3.3 ltr. turbo'd Subaru/350 HP, 25,000 ft., TAS) 383 mph
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Velocity, Never Exceed (Vne) IAS 400 knts/460 mph
Glide Ratio (with all 3 gear UP and prop feathered) 17.5:1
Glide distance in calm winds from 10,000 feet AGL 33+ SM / 28+ NM
(with all 3 gear UP and prop feathered)
Service Ceiling 30,000+ ft.
1170 lb. 2000 lb.
(SL-10K) (SL-10K)
Climb Speed 69-81 mph 91-106 mph
Rate Of Climb (fpm) 3600 2000-1900
Climb Angle 36-30 deg. 14-12 deg.
Engine Out Glide Speed 95-110 mph 124-144 mph
Canard Stall Speed 50-58 mph 65-76 mph
Take-Off & Landing Perf. 1170 lb. @ SL 2000 lb. @ SL 2000 lb. @ 5K ft.
T/O Ground Roll 560 ft. 949 ft. 1205 ft.
T/O Over 50' Obstacle 700 ft. 1387 ft. 1706 ft.
Landing Ground Roll 550 ft. 930 ft.
Landing Over 50' Obstacle 1200 ft. 1745 ft.
WEIGHTS AND LOADINGS:
Gross Weight 2000 lbs.
Empty Weight 900 lbs.
Useful Load 1100 lbs.
Wing Loading (for 2000 lb. GW) 16.051 lbs./sq. ft.
Power Loading (TIO-360 Lyc./210 HP) 9.52 lbs./HP
Fuel (internal) 420 lbs. (70 gal.)
PROPELLER (3 Blades Only):
MT Propeller's constant speed 3 blade prop;
OR Hoffman Propeller's constant speed 3 blade prop;
OR Cato Propellers' wood 3 blade fixed pitch prop
[ POC: Craig Catto at craigcatto@hotmail.com; or call him at (209) 754-3553 ];
OR Performance Propeller's 3 blade fixed pitch prop;
OR Your choice: but 3 blades are ONLY what's recommended.
LANDING GEAR TYPE:
Electro-hydraulic retractable tricycle oleo strut landing gear with
nose wheel steering.
Nose strut kneels the 2200 lb. GW aircraft on it's nose for
easy ingress and egress.
Wheel Base 99.50 in.
Wheel Tread 116.76 in.
Turn-Over Angle (TOA) is only 46 degree's [unlike any other kit canard aircraft, the
only one that is rough terrain capable !]
ENGINE TYPES ( 200 HP is the minimum HP, but maximum allowable engine weight is 400 lbs. ) :
IO-390 220 to 250 HP Lycoming / Superior
OR TIO-360 210 HP Lycoming
OR 3.3 ltr., 6 cyl., 350+ HP Turbocharged SVX Subaru
OR 3.3 ltr., 6 cyl., 260 HP stock SVX Subaru
OR 213 to 225 HP, 4 cyl. Subaru
OR 235 HP, 6 cyl. Continental
OR 240 HP, 6 cyl. Franklin
OR 250 to 350 HP 13B Rotary
OR 350+ HP 20B Rotary
OR 250 to 400 HP Turbo Prop
OR 770 lb. to 1000 lb. thrust Williams Turbo Fan Jet Engine or Pratt & Whitney Turbo Fan Jet Engine
OR Twin 500 lb. or single 1000 lb. thrust Turbo Fan Jet Engines from Lyons Aircraft (615) 604-3854
OR The new diesel engines that are in work / coming out
OR Your Choice: but minimum HP is 200, and maximum engine weight is 400 lbs.
STORAGE AREAS:
Baggage Pods & Pylons -- mounted in wing hard points, pod is removable
from pylon so that different size pods can be used to accommodate golf clubs,
fishing rods, skis, more fuel, fold up scooters, EW, APM, etc.
5+ cu. ft, depending on pod size.
Strakes via front and rear cockpit 20 cu. ft.
DIMENSIONS:
Wing Span 26.83 ft.
Wing Area 112.12 sq. ft.
Canard Span 12.50 ft.
Canard Area 13.72 sq. ft.
Total Canard & Wing Area 125.84 sq. ft.
Overall Length 212.16 in.
Overall Height 92.40 in.
Cockpit Width: Front 27.00 in.
Rear 24.00 in.
Cockpit Height: Front 36.00 in.
Rear 35.00 in.
Cockpit Length: Front 78.00 in.
Rear 62.00 in.
Seats 2, or 3 (2 smaller people in the rear seat)
RDT & E:
770 to 1000 lb. Thrust Turbo Fan Jet Engines 250 to 450 HP Turbo Props
250 to 350 HP Mazda 13B & and 20B Wankel / Rotary Engines
US and foreign Government Interests -- UAV, jet trainer, and as a
manned and / or un-manned attack reconnaissance aircraft. We've done
6 DARPA/Pentagon briefings so far. Call any afternoon CA time for details.
