Infinity 1 Calculated Performance

CALCULATED PERFORMANCE derived from NASA Computer Wind Tunnel Analysis ( within 1 drag count of accuracy ) :

( JD’s goal is to design an entirely new, inexpensive, easy to maintain, fast to build, Quick Build Kit Canard Sport Aircraft with tricycle oleo strut retractable main landing gear, and with steerable retractable oleo nose strut, that will cruise 250+ mph on 210 HP @ 75% power at 10,000 ft., carry 2 people his size [ JD is 6′ 6″ tall ], carry 2 sets of golf clubs and baggage, fly 4+ hrs. and get 20+ mpg, be able to land on grass and dirt runways [ he’s from the Midwest ], and never to land at the same airport twice ( unless there’s something really special at that airport ) so he can see the entire country via the 15,000+ airports in the USA — as you can see, we think we are in there ! )  { No, it will not be sold as a Plans Built Aircraft — sorry. }

Velocity, Never Exceed ( VNE ) IAS	400 knts/h IAS / 460 mph IAS / 740.3 km/h IAS
Glide Ratio ( with all 3 gear UP, and prop stopped and feathered )	17.5 : 1
Glide distance in calm winds from 3,017 feet AGL ( Both examples with all 3 gear UP, and prop stopped and feathered ) Glide distance in calm winds from 10,000 feet AGL ( The average distance between airports in the USA is 15 sm, except in the mountains.  So, on take-off, always zip up to 3000+ feet AGL in less than 2 minutes so that you are always within gliding distance of a runway in case of an engine out situation. )	10+ sm / 8.7+ nm / 16.4+ km 33+ sm / 28+ nm / 53.1+ km
Service Ceiling	30,000+ ft. / 9144 m

Data Points using a 210 hp engine with CS prop	1,170 lbs. ( SL – 10K )	2,000 lbs. ( SL – 10K )
Climb Speed	69 – 81 mph  /  60 – 70.4 knts/h  /  98.2 km/h – 130.4 km/h	91 – 106 mph  /  79.1 – 92.1 knts/h  /  146.5 – 170.6 km/h
Rate Of Climb ( fpm )	3,600	2,000 – 1,900
Climb Angle	36 – 30 deg.	14 – 12 deg.
Engine Out Glide Speed	95 – 110 mph  /  82.6 – 95.6 knts/h  /  152.9 – 177 km/h	124 – 144 mph  /  107.8 – 125.1 knts/h  /  199.6 – 231.7 km/h
Canard Stall Speed	50 – 58 mph  /  43.4 – 50.4 knts/h  /  80.5 – 93.3 km/h	65 – 76 mph  /  65 – 66 knts/h  /  104.6 – 106.2 km/h

Take-Off & Landing Performance with 210 hp engine with CS prop	1,170 lbs. @ SL	2,000 lbs. @ SL	2,000 lbs. @ 5K ft.
T/O Ground Roll	560 ft. / 170.7 m	949 ft. / 289.3 m	1,205 ft. / 367.3 m
T/O Over 50′ Obstacle	700 ft. / 213.4 m	1,387 ft. / 422.8 m	1,706 ft. / 520 m
Landing Ground Roll	550 ft. / 167.6 m	930 ft. / 283.5 m
Landing Over 50′ Obstacle	1,200 ft. / 365.8 m	1,745 ft. / 531.9 m

WEIGHTS AND LOADINGS :

Gross Weight 2,000 lbs.  /  907.2 kg

Empty Weight 900 lbs.  /  408.2 kg

Useful Load 1,100 lbs.  /  499 kg

Wing Loading ( for 2,000 lb. GW ) 15.893 lbs./sq. ft.

Power Loading ( TIO-360 Lyc. / 210 HP ) 9.524 lbs./HP

Fuel ( internal ) 420 lbs. / 190.5 kg ( 70.00 gal. / 265 liters of gas )

PROPELLER ( 3 Blades Only ) :

MT Propeller’s constant speed 3 blade prop ;

OR, Hoffman Propeller’s constant speed 3 blade prop ;

OR, Cato Propeller’s wood 3 blade fixed pitch prop ;

OR, Performance Propeller’s wood 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 2,200 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 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 to IO-405 220 to 250 HP Lycoming ;

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, 700 lb. to 1,000 lb. thrust Williams Turbo Fan Jet Engine , or Pratt & Whitney Turbo Fan Jet Engine ;

OR, Twin 500 lb. or single 700 to 1,000 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.  —  let us know what you install .

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.  /  8.2 m

Wing Area:  112.12 sq. ft.

Canard Span:  12.50 ft.  /  3.8 m

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 1,000 lb. Thrust Turbo Fan Jet Engines ; or, 250 to 450 HP Turbo Props

250 to 350 HP 13B, and 20B, Mazda Rotary Engines

US and Foreign Government interests have contacted us for:  Turn-Key light attack jets, and jet trainers; and for Turn-Key manned and / or un-manned attack reconnaissance UAV aircraft.  In fact, we’ve given 6 briefings to DARPA and the Pentagon at their request.  Call any afternoon M-F after 1330 CA time for more details.