IO Aircraft - Chippewa SC - 24 Passenger + 3 Crew Suoer eVTOL Hybrid

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Chippewa SC - 24 Passenger + 3 Crew Medium Lift eVTOL Hybrid

 

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Passengers:

24 Personnel

3 Crew
Total Length: 47'

Total Span:

41.5'

Power:

Kero (Jet A, JP7/8) + Hydrogen Fuel Cell

Propulsion:

6X Superconducting Graphene Based EDF's

2X U-GTG (Unified Thrust Produce Gas Turbine Generators)

Range:

1,000+ NM Kero or H2 Exclusively

3,000 NM, Both Simultaneously at altitude

Performance:

 

450 KT Cruise

500+mph gs at 30,000ft

Safety:

 

Aircraft also equipped with a BRS (Ballistic Recovery System)
  Estimate Price in Production $6 Million Fly Away Price not including advanced avionics/systems.

 


Chippewa SC - 24 Passenger + 3 Crew Medium Lift VTOL Fixed Wing Aircraft

 

 

*This aircraft design is not a graphics concept, but ready to be built and begin certification processes leading into serial production

Chippewa SC is for defense sector only, commercial version is completely hydrogen fuel cell. At 47' length, the aircraft is 3' shorter length then a UH-60 Blackhawk, but the same bay dimensions as a V-22 Osprey, with an addition 6" cabin width at 36" above the cabin floor.  There is also a fwd cabin for the crew chief, lavatory accommodations, and systems/ammunition stores.


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This aircraft is designed as a super vtol medium lift. In the class of UH-60 Blackhawk's and extensively superior to the Sikorsky V-280 (320mph top speed), except in military configuration double the capacity and a smaller footprint and substantially heavier lift capabilities, along with a split rear payload door.

Control surface on the wings are not hinged, but wing warping surfaces with precision control, allowing for advanced flow of the air stream for optimized performance.

The entire airframe for this aircraft is produced using GRAPHENE and composites with an overall 33X greater strength then titanium but 1/100th the weight, it is also bulletproof through 20mm. The entire airframe stripped, could be lift by hand from 1 person.

  • Overall, the aircraft weight fueled, is less then a UH-60 empty.

 

Propulsion for Chippewa SC are via twin U-GTG turbines, which are unified gas turbine generators. These engines, the core of the turbine assembly are super conducting graphene based generators, which for this aircraft would have apx 500kw power output each, without any loss of thrust from thr turbine assemblies.

 

The other 6 units, are Graphene based superconducting edf's (electric ducted fans) which are able to provide apx 1:1 thrust compared to turbines (jet engines) of comparable scale.

  • Additionally, The propulsion system comes equipped with Io Aircraft's own high performance vtol capabilities via rotating composite nozzles.  It should be noted, Lockheed Martin did not invent rotating nozzles, their own for the F-35 are their own style, but the technology was actually originally developed for the soviet era Yak-141.  We have developed our own style using that as a baseline principle.  The main difference is these are much higher technology levels, and high speed capabilities.

Turbines can operate on Compressed Hydrogen or Kero, or a combine of both simultaneously. This results in either very long range capabilities, or mission specific.

  • Additionally, this aircraft is aerial refueling equipped, but integration for both basket and probe type refueling capabilities are built in, for total inter service and nato operations globally. No variation is then required.

Performance of Chippewa SC is extreme, and is able to match the UH-60 Blackhawk capabilities in both slow flight and hover.

  • This includes radical maneuvering

 

Important Aircraft Features

Chippewa SC is capable of massive weapons and utility capabilities.

  • Utility

  • Sling Load over 10,000 LBS

  • Medivac/Mobile Hospital

  • Laser Weapons Platform

  • Gunship / Pavelow

    • 1+ Megwatt Laser Capabilities, Up to 8 AGM-118 Hellfire's or any similar of armament, 3 retracting Gau-17 7.62mm Mini Guns that are remotely operated via the pilots or crew chief, with precision targeting capabilities provides a 360° down range coverage,
       

  • High Intensity Troops infiltration/infiltration under direct fire.

  • All weather conditions
     

  • Folding Wings for minimal ground footprint when parked or stored, including maritime operations

  • Split Rear Payload Door

  • Up to 18 Stretchers Configured for Medivac

  • Graphene & Composite Airframe (lower costs then aluminum, 33X stronger then Titanium, 1/100 the weight

  • Dual Kero and Hydrogen Fueled, can operate on either, or both

  • If turbine failure occurs then the Fuel Cell Stacks provides several minutes to land safely, or vice/versa

  • Ballistic Recovery System Built In.

  • Advanced fly by wire system providing high performances capabilities
     

  • Aggressive maneuvering in both high speed and low speed flight. Chippewa SC is able to fly in low level harsh terrain, highly aggressively on par with attack/fighter aircraft and sustained 9+ G.
     

    • And a byprodct of the vast capabilities, Chippewa SC is additionally able to provide enormous ground support similar to an A-10 Thunderbolt

     

  • Chippewa SC is able to land and take off conventionally, STOL (short landing and take off), and VTOL (vertically take off and landing) at max load of 24 troops each with over 100 lbs of gear, plus pilots and crew chiefs at above 5,000ft density altitude.  
     

Because of the Graphene airframe composition and High Pressure H2 tanks; this aircraft in maritime operations cannot sink, if catastrophic failure occurs, resulting in impact with water or ditching the aircraft remains buoyant.

If the aircraft suffers catastrophic damage or total failure at an altitude above 500' agl, BRS will deploy and the entire aircraft will descend via parachute.

 

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