Creating a New Category in Light Jets: A dva n c e d
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E N G I N E E R E D
F O R
P erfor m a n c e
An all-composite fuselage, a natural-laminar flow airfoil and nose design, and an over-the-wing engine configuration combine to enable the highest speed and best fuel efficiency in its class.
D E S I G N E D
F O R
D E S I R E
The preferred execution of onboard comfort includes a spacious, elegantly appointed cabin, a fully private lavatory, and generous cargo stowage.
B u i l t
for
P erfe c tion
Innovative design, exacting development, and meticulous testing result in a new class of light jet: Advanced.
T h e
S k y
I s
Yo u rs
Advanced engineering
D E S I G N
I N NOVAT ION
for performance and passenger comfort
Over-the-Wing Engine-Mount Design
HondaJet’s Over-the-Wing Engine-Mount (OTWEM) design solves two challenges, beautifully: It achieves wave-drag reduction so efficiently, it actually out-performs clean-wing designs. It eliminates engine-mount fuselage encroachment for a larger, more spacious cabin and greater cargo stowage capacity. Jet owners no longer have to decide between performance and comfort. HondaJet delivers both.
Remarkable performance
Extraordinary comfort
High cruise efficiency
Expanded cabin space
DESIGN
I N N O VATI O N
Advanced engineering for performance
N a t u r a l - L a m i n a r F l ow A i r fo i l a n d No s e
The HondaJet Natural-Laminar Flow (NLF) airfoil and nose design boosts fuel efficiency and improves performance, simultaneously: It exhibits a high maximum lift coefficient and low profile drag coefficients at climb and cruise, resulting in high fuel efficiency and class-leading performance. It results in a small nosedown pitching moment coefficient at high speeds and reduced loss in maximum lift coefficient due to leading-edge contamination, providing responsive and reassuring handling characteristics.
Exceptional efficiency
Outstanding responsiveness
High maximum lift coefficient
Docile stall characteristics
and efficiency
Advanced engineering
D E S I G N
I N NOVAT ION
for performance and reliability
GE / H O N D A H F 1 2 0 T u r b of a n E n g i n e
GE/Honda HF120 Turbofan engines power HondaJet to new levels of performance for range, payload, and dependability: Fluid dynamics software automatically optimizes airflow for maximized performance. Full Authority Digital Electronic Control (FADEC) system provides superior reliability and optimal operation.
Unparalleled dependability
Rewarding performance
Ultra-compact FADEC
High thrust-to-weight ratio
DESIGN
I N N O VATI ON
Advanced engineering in aviation fuselage
A l l - C om p o s i t e F u s e l a g e
A remarkably light all-composite fuselage is one reason HondaJet offers both exceptional fuel efficiency and performance – and its structure allows for a more spacious cabin, as well: A cutting-edge combination of co-cured integral structure and honeycomb sandwich structures produces a lighter fuselage design that contributes to greater fuel efficiency and increased performance. The advanced fuselage configuration contributes to a larger interior cabin space for greater comfort and increased payload.
Performance-focused structure
Space-conscious design
Fast, yet fuel efficient benefits
Room to relax
design
SPE C I F I C ATI O NS
P erfor m a n c e Maximum Cruise Speed @ FL300
420KTAS
Service Ceiling
FL430
Rate of Climb
3990 ft/min
VFR Range
1400 nm
IFR Range
1180 nm
Take-off Distance
3120 ft
Landing Distance
2500 ft
E ngines Manufacturer / Model
GE-HONDA / HF120
Output
1880 lb/each
Bypass Ratio
2.9
E x tern a l
D i m ensions
Height
13.21 ft [4.03 m]
Length
41.70 ft [12.71 m]
Span
39.87 ft [12.15 m]
Pay l o a d Passengers
2 crew + 5 passengers
Baggage
66 cu.ft
HondaJet Engineered for Performance | Designed for Desire | Built for Perfection
hondajet.com
HondaJet Engineered for Performance | Designed for Desire | Built for Perfection
hondajet.com