| Manufacturer |
McDonnell Douglas |
Glenn L. Martin Company |
| Description |
The McDonnell Douglas YC-15 is a prototype four-engine short take-off and landing (STOL) tactical transport. |
The Martin P7M was an unbuilt aircraft designed by the Glenn L. |
| ICAO Code |
C15 |
|
| First Flight |
1975-08-26 |
|
| Designer |
McDonnell Douglas |
Glenn L. Martin Company |
| Type |
Tactical airlifter |
|
| Length (m) |
37.9 |
41.4528 |
| Height (m) |
13.2 |
11.8872 |
| Cockpit Crew |
3 |
|
| Max Seating |
150 |
|
| Max Speed (km/h) |
950 |
648.1994 |
| Cruise Speed (km/h) |
872 |
|
| Max Ceiling (m) |
9100 |
7711.44 |
| Armament |
|
Missiles, bombs, and depth charges on external hard-points |
| Capacity Description |
Up to 150 troops or 78000 lb of cargo |
|
| National Origin |
United States of America |
Canada |
| Number Built |
2 |
0 |
| Powerplant Description |
4 × Pratt & Whitney JT8D-17 turbofans, 72.5 kN thrust each |
4 × Wright R-1820-42 radial piston engines, 1137 kW (1525 hp) each |
| Primary Users |
|
United States Navy |
| Status |
Cancelled |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/McDonnell_Douglas_YC-15 |
en.wikipedia.org/wiki/Martin_P7M_SubMaster |
| Flat Wing Span (m) |
33.6 |
33.8328 |
| Flat Wing Area (m²) |
160 |
232.2576 |
| Wake Category |
M |
|
| Aircraft Engine |
Pratt & Whitney JT8D |
|
| Number of Engines |
4 |
4 |