Airbus Helicopters H145 vs Gulfstream G650er
The Airbus Helicopters H145 is a twin‑engine light utility helicopter designed for short‑range, point‑to‑point missions such as emergency medical services, law enforcement, and corporate shuttle work where vertical takeoff and landing are essential. Its typical operational range is on the order of a few hundred nautical miles (roughly 300–350 nm depending on configuration and reserves). Passenger capacity varies by layout, but it commonly carries a pilot plus about 6–9 passengers, with some seating arrangements allowing up to around 10 occupants including crew. The Gulfstream G650ER is an ultra‑long‑range business jet built for high‑speed intercontinental travel between major airports. It offers a published range of about 7,500 nautical miles, enabling nonstop flights such as New York to Hong Kong under favorable conditions. Cabin capacity is generally configured for business travel, typically seating about 11–18 passengers (with certified maximum occupancy higher depending on interior and regulations), and it cruises far faster and higher than a helicopter, trading VTOL flexibility for vastly greater range and speed.
| Spec | AIRBUS H145 | Gulfstream G650ER |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 9.31 | $ 9.39 |
| Min Crew | 1 | 4 |
| Total Seats | 10 | 14 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Gulfstream |
| Aircraft Name | H145 | G650ER |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 7500 |
| DOC / nm / Seat | $ 0.93 | $ 0.78 |
| Max Cabin Seats | 9 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 49500 |
| Standard Cabin Seats | 8 | 12 |
| Direct Operating Cost | $ 1,210 | $ 4,844 |
| Flight Deck (Base Spec) | EFIS | Gulfstream PlaneView II (Primus Epic) |
| Max Cruise Speed (ktas) | 130 | 516 |
| Base Aircraft Price (USD) | $10,200,000 | $60,000,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 4 |
| Total Seats | 10 | 14 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 9 | 19 |
| Standard Cabin Seats | 8 | 12 |
| Lavatory | — | 2 Enclosed Flushing |
| Crew Rest | — | Yes |
| Jump Seat | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD / AFT |
| Cabin Pressure (psi) | — | 10.7 |
| Galley / Refreshment | — | Galley |
| SL Cabin Altitude (ft) | — | 31900 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Arriel 2E | BR725 A1-12 |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 4000 | On-Condition |
| Horsepower | 894 | — |
| No. of Engines | 2 | 2 |
| Flat Rating | — | ISA + 15 |
| Thrust (lbs) | — | 16900 |
| Dimensions | ||
| Length (ft) | 44.8 | 99.8 |
| Overall Height (ft) | 13 | 25.7 |
| Rotor Diameter (ft) | 36.1 | — |
| Cabin Volume (cu. ft) | 166 | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | — |
| Wingspan (ft) | — | 99.6 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Width (ft) | — | 8.2 |
| Cabin Height (ft) | — | 6.5 |
| Cabin Length (ft) | — | 46.9 |
| Cabin Width - Floor (ft) | — | 6.7 |
| Cabin Length - Seating (ft) | — | 32.7 |
| Baggage Volume Int. (cu. ft) | — | 235 |