Stratus Design Company
| Type | Private, government subsidized |
|---|---|
| Industry | Aviation |
| Founded | 1719 AN |
| Headquarters | Boulonne, Meckelnburgh |
| Number of locations | 2 offices, 1 manufactory |
| Area served |
 Meckelnburgh |
| Products | Trainer aircraft |
| Owner(s) |
Stratus Design Co. (55%) Government of Meckelnburgh (45%) |
| Website | stratusaircraft.mb |
The Stratus Design Company, also known as Stratus Aircraft, is a aircraft manufacturing and design company headquartered in Boulonne, Meckelnburgh. Founded in 1719 AN with a grant from the Ministry of Defense Affairs, Stratus Aircraft specializes in the design of trainer aircraft for military and government usage. Its main manufacturing plant is located in Victoria, Meckelnburgh. The company relies on a 45% ownership subsidy from the Meckelnburgh government.
Stratus Aircraft is expected to deliver its first shipment of aircraft in 1724 AN, the piston-engine T-1 Débutants, to the Royal Meckelnburgh Air Force. The second generation of turbo-piston and turboprop trainers is expected to begin delivery in 1726 AN with the T-2 Apprenants and T-3 Étudiants. The company hopes to introduce its first generation of twin-engined jet trainers, the T-110 Apprentis and T-120 Cadets, in 1733 AN.
Products
| Name | Purpose | Crew/Cap. | Empty weight | Powerplant | Max speed | Range | Ceiling | Production | Image |
|---|---|---|---|---|---|---|---|---|---|
| Piston engine | |||||||||
| T-1 Débutants | Elementary trainer | 2 / 2 | 670 kg | 4-cylinder piston | 130 kn | 620 nmi | 6,100 m | 1724 AN– | |
| T-2 Apprenants | Primary trainer | 1 / 4 | 1,029 kg | 6-cylinder turbo-piston | 220 kn | 1,050 nmi | 5,300 m | 1726 AN– | |
| Turboprop | |||||||||
| T-3 Étudiants | Turboprop trainer | 1 / 2 | 1,095 kg | Turboprop engine | 245 kn | 580 nmi | 7,600 m | 1726 AN– | |
| Twin-engined jet | |||||||||
| T-110 Apprentis | Airlift trainer | 2 / 3 | 4,740 kg | 2 × turbofan | 470 kn | 2,900 nmi | 12,000 m | 1733 AN– | |
| T-120 Cadets | Dual-jet trainer | 2 / 2 | 4,635 kg | 2 × turbojets | 520 kn | 600 nmi | 13,700 m | 1733 AN– | |
Conception-phase
| Name | Purpose | Crew/Cap. | Empty weight | Powerplant | Max speed | Range | Ceiling | Production | Image |
|---|---|---|---|---|---|---|---|---|---|
| T-130 Stagiaires | Single-jet trainer | 2 / 2 | 4,480 kg | 1× turbofan | 555 kn | 1,400 nmi | 13,600 | Unknown |
