| Manufacturer |
Berliner-Joyce |
AviaBellanca Aircraft Corporation |
| Description |
The Berliner-Joyce P-16 was a 1930s United States two-seat fighter aircraft produced by Berliner-Joyce Aircraft Corporation. |
The Bellanca 19-25 Skyrocket II was a prototype light airplane built in the United States in the 1970s. |
| First Flight |
1930-09-01 |
1975-03-01 |
| Entry Into service |
1932-01-01 |
|
| Service End |
1940-01-01 |
|
| Designer |
Berliner-Joyce |
AviaBellanca Aircraft Corporation |
| Type |
Two-seat fighter |
Utility aircraft |
| Length (m) |
8.59 |
8.2296 |
| Height (m) |
3.1 |
2.7432 |
| Cockpit Crew |
2 |
|
| Max Speed (km/h) |
282 |
532.6929 |
| Cruise Speed (km/h) |
|
410.3827 |
| Min Speed (km/h) |
|
104.6074 |
| Max Ceiling (m) |
|
9144 |
| Rate of Climb (m/s) |
|
9.652 |
| Armament |
two fixed forward-firing and one flexible-mounted 0.3 in (7.62 mm) machine guns, maximum bombload of 224 lb (102 kg) |
|
| Capacity Description |
|
five passengers |
| Number Built |
26 |
|
| Powerplant Description |
1 × Curtiss V-1570-25 Conqueror inline piston, 447 kW (599 hp) each |
1 × Continental GTSIO-520-F air-cooled flat-six, 324 kW (435 hp) each |
| Primary Users |
United States Army Air Corps |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Berliner-Joyce_P-16 |
en.wikipedia.org/wiki/Bellanca_Skyrocket_II |
| Flat Wing Span (m) |
10.36 |
10.3632 |
| Flat Wing Area (m²) |
27 |
16.9641 |
| Flat Wing Aspect Ratio |
|
6.667 |
| Aircraft Engine |
|
Continental IO-520 |
| Number of Engines |
1 |
1 |