baseline mtcr 1 mtcr 2 mtcr 1 mtcr 2 · 2019. 4. 9. · powerplant: single turbomeca arriel 2n...

• Internal Cargo Volume 5,500 Liter (190 ft^3)

MTCR 2Wing

MTCR 2Car

go L

oad

- Kg

Baseline

* Design A

Wing + 2nd Engine **

MTCR 1Wing *

MTCR 2

MTCR 1

Wing **

** Design B

• Powerplant: Single Turbomeca Arriel 2N Turboshaft • (985 SHP Uninstalled T.O. Power @ S.L. ISA) • Vertical Take-Off and Landing (VTOL) • Certified to MTCR Category 2• Basic Empty Wt. ………….................…..977 kg (2,150 lb) • Max T.O. Wt. …………………………....1,741 kg (3,830 lb) • Payload + Useful Fuel Wt ………...........764 kg (1,680 lb) • Mission Wt. (440kg payload Ref) ........1,520 kg (3,344 lb) • Max Speed .......................................... 180 Km/hr (100 Kt) • Fuel Flow @ Mission Wt; 90 Kt *…….....208 kg/hr (458 lb/hr) • Endurance (300kg Payload (Ref)) ……2.6 hrs • Payload-Range ………………………... (see chart)

Note: Mission Wt = Basic Empty Wt + Payload +½ Fuel

* @ Sea Level (Best Range Altitude); ISA

Preliminary data, specifications are subject to change without notice

Cormorant

Wing drawing for Ref only

Internal width=2.4m

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