Ilyushin Il-108
| Industry | Aerospace |
|---|---|
| Founded | 1933 |
| Headquarters | Moscow , Russia |
The Ilyushin Il-108 was a conceptual twin-engine business jet designed by the Russian company Ilyushin in 1990. Although a prototype was unveiled that same year, it appears that the Il-108 never achieved any flight tests. Its external design bears resemblance to the Canadair Challenger 300.
Design
Two configurations were proposed: a nine-seat executive model and a 15-passenger commercial variant. Both featured a low-wing layout combined with a T-tail structure. Propulsion came from a pair of Lotarev DV-2 turbofan engines mounted atop the rear fuselage flanking the tail assembly, each delivering approximately 21.6 kN of thrust.
Variants
An alternative iteration was intended to utilize Lotarev DV-22 turbofan engines, which offered a bypass ratio of 5 and increased thrust rated at 35 kN.
Specifications
{{Aircraft specs |ref=Template:Fix/category[citation needed] |prime units?=met |crew=2 |capacity=1,600 kg (3,527 lb) payload / 9-15 passengers |length m=15.85 |length note= |span m=15 |span note= |height m=5.5 |height note= |wing area sqm= |wing area note= |aspect ratio= |empty weight kg= |empty weight note= |gross weight kg= |gross weight note= |max takeoff weight kg=14300 |max takeoff weight note= |fuel capacity= |more general= |eng1 number=2 |eng1 name=Lotarev DV-2 |eng1 type=turbofan engines |eng1 kn=21.6 |eng1 note= |max speed kmh= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed note= |stall speed kmh= |stall speed note= |never exceed speed kmh= |never exceed speed note= |min control speed kmh= |min control speed note= |min control speed kmh= |min control speed note= |min control speed kmh= |min control speed note= |min control speed kmh= |min control speed note= |min control speed kmh= |min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|min control speed kmh=
|min control speed note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
|max takeoff weight kg=14300
|max takeoff weight note=
|
- Please disregard the repetition above; it is an error.
- Corrected version: