| Manufacturer |
Glenn L. Martin Company |
| Description |
The Martin 2-0-2 was a low-wing, all-metal, twin piston-engined American airliner designed and built by the Glenn L. |
| First Flight |
1946-11-22 |
| Entry Into service |
1947-01-01 |
| Production End |
1948-01-01 |
| Service End |
1975-01-01 |
| Designer |
Glenn L. Martin Company |
| Type |
Airliner |
| Length (m) |
21.6408 |
| Height (m) |
8.5344 |
| Cockpit Crew |
2 |
| Max Seating |
40 |
| Max Speed (km/h) |
500.506 |
| Cruise Speed (km/h) |
471.5378 |
| Min Speed (km/h) |
122.3101 |
| Max Ceiling (m) |
10058.4 |
| Rate of Climb (m/s) |
11.176 |
| Capacity Description |
; 40 passengers or; 9270 lb payload |
| National Origin |
Canada |
| Number Built |
47 |
| Powerplant Description |
2 × Pratt & Whitney R-2800 CA-18 Double Wasp 18-cylinder air-cooled radial engine, 1342 kW (1800 hp) each |
| Primary Users |
Northwest Orient Airlines, LAN Chile , Trans World Airlines |
| Status |
Retired |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Martin_2-0-2 |
| Flat Wing Span (m) |
28.3464 |
| Flat Wing Area (m²) |
80.2682 |
| Number of Engines |
2 |