DART SERIES - Diamond Aircraft · 2018-10-25 · From the very beginning, Diamond Aircraft knew...
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DART SERIES THE NEXT LEVEL OF VERSATILITY
Transcript of DART SERIES - Diamond Aircraft · 2018-10-25 · From the very beginning, Diamond Aircraft knew...
DART SERIES THE NEXT LEVEL OF VERSATILITY
From the very beginning, Diamond Aircraft knew that the DART series will be something unmatched on the market and will eliminate old generation trainer from the market for a very long period of time.
general information The DART will be the world‘s first civil certified all-carbon fiber tandem, 2-seat aerobatic trainer with sidestick control and ejection seats. ENGINE VARIANTS ▪ Turboprop engine AI-450 SR (450 hp) manufactured by Motor Sich for DART-450 ▪ Turboprop engine GE H75-100 (550 hp) manufactured by General Electric for DART-550 ▪ Airframe is designed to accommodate a power plant up to 1000 hp KINDS OF OPERATION ▪ Daytime flights according to Visual Flight Rules (VFR) ▪ Night flights according to Instrument Flight Rules (NVFR) ▪ Flights according to Instrument Flight Rules (IFR) ▪ Take-off and landing on paved surfaces or grass surfaces ▪ Flights into known or forecast thunderstorms or icing conditions APPLICATIONS Flight training, Aerobatic, Formation, Utility STRUCTURE All composite aircraft CFRP (Carbon Fiber Reinforced Polymer monolithic and sandwich structures). CERTIFICATION STANDARD EASA CS 23 CATEGORY Aerobatic / Utility (Multi Role) Page 3
FROM CONCEPT TO PRESENT
MOCK UP DART-450DEC 2015
KICK OFF DART-450MAY 2015
ROLL OUT DART-450APRIL 2016
MAIDEN FLIGHT DART-45017 MAY 2016
MAIDEN FLIGHT DART-55003 MAY 2018
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DART FEATURESTANDEM SEAT, SIDE STICK CONTROL,
EJECTION SEATS, TOUCH SCREEN AVIONICS
HOTAS, NVIS
LARGESTINTERNAL FUEL TANK
CAPACITY IN TRAINER CLASS
8 HRS + ENDURANCE
LEADING EDGE DE - ICE SYSTEM
MOST AERODYNAMICSHAPE FOR HIGH SPEED
TRAINING MANEUVERS
5 BLADE PROPELLER POWERED BY
FUEL & COST EFFICIENT TURBINE
EXTREME ROBUST LANDING GEARFOR UNPAVED SURFACE OPERATION
PROVEN HIGH SPEED WING
(WIND TUNNEL TESTED UP TO M0.65)
DOUBLE SLOTTED FLAPS
FOR MAXIMUM LIFTEXTREMELY LOW STALL SPEEDS
SHORTEST LANDING DISTANCES
15’’ CAMERA HATCH FOR
MULTI ROLE OPERATION
BIRD STRIKE PROOF CANOPY
WITH EXTRAORDINARYSURROUND VIEW
dart FEATURES
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DART VARIANTS
The DART-550 is the next massive push into being the only aircraft manufacturer in offering the full range for basic flight training, reaching its peek with this soon fully EASA certified DART-550 aerobatic trainer.
DART-450 Turboprop engine AI-450 SR (450 hp) manufactured by Motor Sich.
DART-550 Turboprop engine GE H75-100 (550 hp) manufactured by General Electric.
AEROBATIC CONFIGURATION 1)
Load factor +7 / -4,0
MTOM 2,080 kg / 4,586 lbs
UTILITY (MULTI ROLE) CONFIGURATION 1)
Load factor +5 / -2,4
MTOM 2,400 kg / 5,291 lbs
DART-450 KEY FACTS:
Max. Take-off power495 HP or 369 kW
Load Factor+7 / -4
Max. Speed370 km/h or 200 kts
Endurance 8 hours +
DART-550 KEY FACTS:
Max. Take-off power550 HP or 404 kW
Load Factor+7 / -4
Max. Speed491 km/h or 265 kts
Endurance 8 hours +
1) Applies to the complete DART Series
Having the opportunity to include state of the art glass cockpit technology, world’s number one ejection seat brand, using General Electric turbine know-how - embedded in a full carbon fiber airframe will make it very difficult for DART’s competition when performance and commercial arguments become a critical decision making factor.
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AVIONICS Garmin G3000 dual glass cockpit: ▪ Touchscreen control ▪ Synthetic Vision Technology (SVT™) ▪ 14.1-inch diagonal WXGA high-resolution cockpit displays ▪ 5.7-inch high-resolution GTC 570 ▪ Extended 16:9 width-to-height ratio Alternative avionic suites on request. COCKPIT ▪ Bird strike proof canopy ▪ Enhanced cockpit surround view ▪ Real and fully independent tandem cockpit concept ▪ Revolutionary simplified ejector seat concept ▪ Electrical adjustable seat height
COCKPIT & EJECTION SEATS
EJECTION SEAT CONFIGURATION Martin Baker MK16 Lightweight Escape System: ▪ JPATS (Joint Primary Aircraft Training System) multi variate body size cases 2 to 7 ▪ Minimal maintenance overhead ▪ 65 kg mass per seat + 8 kg ground survival equipment ▪ Electric height adjustment system ▪ Speed range 0 KIAS – 370 KIAS ▪ Altitude 0 ft – 50,000 ft ▪ Pilot Mass: 62.3 kg - 123 kg Alternative: Zwezda KC-2012
AEROBATIC TRAINING
(smoke on aerobatic flight)
ADVANCED TRAINING Powered by the General Electric GE H75-100 turboprop engine with 550 hp or the Motor Sich AI-450 SR turboprop engine with 450 hp. This engine variants combined with operating simplicity makes it the ideal platform for learning the first steps of flying all the way to pushing the envelope at +7g / -4g during the aerobatic training phase.
ONE AIRPLANE - TWO CONFIGURATIONS ▪ With partial fuel (350 l) the airplane can be operated within the aerobatic category ▪ With full fuel (826 l) the airplane can be operated within the utility (mulit role) category
The DART aerobatic trainer will be available in different vari-ants differing in engine power ratings, seat configuration and/or avionics options for diverse customer needs.
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AEROBATIC TRAINING
UTILITY (MULTI ROLE)
ADDITIONAL ATTACHMENT POINTS ▪ Fuselage: Large attachment area for external payloads up to 225kg / 500lbs ▪ Wing: Hard points for external payload up to 225kg / 500lbs per store.
UTILITY (MULTI ROLE)
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THE NEXT LEVEL OF VERSATILITY
DART-450 FACTS AND SPECIFICATIONSPower plant
Engine Motor Sich AI-450 SR turboprop engine
PropellerMT propeller MTV-5-1-E-C-F-R(P) 5-blade with feathering and reverse functionality
Fuel gradesJet A-1, Jet A, TS-1 (Russia, Ukraine), RT (Russia, Ukraine), No. 3 Jet Fuel (China), JP-8
Dimensions / mass / loading
ConfigurationAerobatic Configuration
Utility (Multi Role) Configuration
Load factors +7 / -4 +5 / -2.4
Maneuvers Aerobatic Cat. Utility Cat.
MTOM2,080 kg /4,586 lbs
2,400 kg /5,291 lbs
Basic empty mass1,450 kg /3,196 lbs
1,550 kg / 3,417 lbs
Max. usable fuel240 kg or 300 ltr / 529 lbs or 79 US gal
662 kg or 826 ltr /1,459 lbs or218 US gal
Seats 2 2
Calculated Performance
Max. take off power 495 HP 369 kW
Max. continuous power (ISA, SL) 400 HP 298 kW
Expected top speed (12.000 ft, MCP, 114 kg/h)
370 km/h TAS 200 KTAS
Typical cruise speed (10.000ft, 75%, 97 kg/h)
352 km/h TAS 190 KTAS
Endurance 8 hours + 8 hours +
Max. rate of climb 8.9 m/s 1,750 ft/min
Service ceilling 7,000 m 23,000 ft
Take-off distance (ISA, SL) ≤ 600 m ≤ 1,970 ft
Landing distance (ISA, SL) ≤ 400 m ≤ 1,300 ft
9.75 m / 34 ft
3.43 m / 11 ft 3 in
11.79 m / 38 ft 8 in
The above quoted data are preliminary specifications and may change without notice.
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DART-550 FACTS AND SPECIFICATIONSPower plant
Engine General Electric GE H75-100 turboprop engine
PropellerMT propeller MTV-5-1-E-C-F-R(P) 5-blade with feathering and reverse functionality
Fuel gradesJet A-1, Jet A, TS-1 (Russia, Ukraine), RT (Russia, Ukraine), No. 3 Jet Fuel (China), JP-8
Dimensions / mass / loading
ConfigurationAerobatic Configuration
Utility (Multi Role) Configuration
Load factors +7 / -4 +5 / -2.4
Maneuvers Aerobatic Cat. Utility Cat.
MTOM2,080 kg /4,586 lbs
2,400 kg /5,291 lbs
Basic empty mass1,500 kg / 3,307 lbs
1,600 kg / 3,527 lbs
Max. usable fuel240 kg or 300 ltr / 529 lbs or 79 US gal
662 kg or 826 ltr /1,459 lbs or218 US gal
Seats 2 2
Calculated Performance
Max. take off power 550 HP 404 kW
Max. continuous power (ISA, SL) 550 HP 404 kW
Expected top speed (20.000 ft, MCP, 159 kg/h)
491 km/h TAS 265 KTAS
Typical cruise speed (10.000ft, 60%, 95 kg/h)
352 km/h TAS 190 KTAS
Endurance 8 hours + 8 hours +
Max. rate of climb 10.7 m/s 2,100 ft/min
Service ceilling 7,600 m 25,000 ft
Take-off distance (ISA, SL) ≤ 600 m ≤ 1,970 ft
Landing distance (ISA, SL) ≤ 400 m ≤ 1,300 ft
9.75 m / 34 ft
3.43 m / 11 ft 3 in
11.79 m / 38 ft 8 in
The above quoted data are preliminary specifications and may change without notice.
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EUROPE, MIDDLE EAST, AFRICA, RUSSIA/CIS, ASIA PACIFIC (HQ):N. A. Otto-Strasse 5, 2700 Wiener Neustadt, AustriaPhone: +43 2622 26700, [email protected]
NORTH AMERICA & SOUTH AMERICA:1560 Crumlin Sideroad, London, ON, Canada, N5V1S2Phone: +1 888 359 3220, [email protected]
CHINA:Wanfeng Airpark, Dashiju Town Xinchang County, Zhejiang Province, P. R. China
AVIATION AS UNIQUE AS YOU ARE
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© 2018 Diamond Aircraft Industries GmbH. Data is subject to change without prior notification. Images may show optional equipment or experimental aircraft. 07/2018 S_00002E
