Technológia
Over-the-wing Engine Mount Configuration
Engine location was the major design decision in the development of the HondaJet configuration. Conventional wisdom suggests that locating the engine nacelles over the wing creates unfavorable aerodynamic interference, inducing a strong shock wave that increases drag. However, through experimentation and extensive testing, Honda engineers discovered an optimal position for the nacelle over the wing that minimizes the shock wave and achieves lower drag than the conventional rear-fuselage engine mount configuration. And, since the engine support structure does not go through the fuselage, fuselage internal volume is maximized.
Specifikáció
| Maximum Cruise Speed @ FL300 | 420KTAS |
| Service Ceiling | FL430 |
| Pressurization (Differential) | 8.7 psi |
| Range Performance | |
 VFR Range (Maximum fuel with available payload (644lb)) |
1400 nm |
| IFR Range
|
1180 nm |
| Rate of Climb | 3990 ft/min |
| Airport Performance | |
| Take-off Distance* |
3120 ft |
| Landing Distance |
2500 ft |
| Engines | |
| Manufacturer / Model |
GE-HONDA / HF-120 |
| Output |
1880 lb/each (Max Take-Off) |
| Bypass Ratio |
2.9 |
| External Baggage Capacity | |
| Nose Baggage |
9 cu.ft |
| Aft Baggage |
57 cu.ft |
| External Dimensions | |
| Height |
13.21 ft (4.03 m) |
| Length |
41.70 ft (12.71 m) |
| Span |
39.87 ft (12.15 m) |
| Cabin Dimensions | |
| Height |
4.94 ft (1.51 m) |
| Length—Fwd. Pressure Bulkhead to Aft Pressure Bulkhead |
17.80 ft (5.43 m) |
| Width |
5.00 ft (1.52 m) |
| Seating | |
| Typical |
2 crews + 5 passengers |
Video
