CAC CA-15: Perbedaan antara revisi

Konten dihapus Konten ditambahkan
Baris 46:
* '''Powerplant:''' 1 × [[Rolls-Royce Griffon 61]] V-12 liquid-cooled piston engine, 2,035 hp (1,517 kW) with 18 psi (120 kPa) boost
* '''Propellers:''' 4-bladed [[Rotol]], 12 ft 6 in (3.81 m) diameter constant-speed propeller
 
<span style="font-size:120%">'''Performance'''</span>
 
* '''Maximum speed:''' 442&nbsp;mph (711&nbsp;km/h, 384&nbsp;kn) at 25,600&nbsp;ft (7,800&nbsp;m) and 368&nbsp;mph (320&nbsp;kn; 592&nbsp;km/h) at sea level
* '''Range:''' 1,150&nbsp;mi (1,850&nbsp;km, 1,000&nbsp;nmi) on internal fuel
* '''Ferry range:''' 2,540&nbsp;mi (4,090&nbsp;km, 2,210&nbsp;nmi) at 5,000&nbsp;ft (1,500&nbsp;m) at 1,600 rpm
* '''Service ceiling:''' 34,000&nbsp;ft (10,000&nbsp;m)
* '''Rate of climb:''' 4,900&nbsp;ft/min (25&nbsp;m/s)
* '''Time to altitude:''' 20,000&nbsp;ft (6,100&nbsp;m) in 5 minutes 30 seconds
* '''Wing loading:''' 37.5&nbsp;lb/sq&nbsp;ft (183&nbsp;kg/m<sup>2</sup>) normal load
 
:: 48.8&nbsp;lb/sq&nbsp;ft (238.3&nbsp;kg/m<sup>2</sup>)
 
* '''[[Power-to-weight ratio|Power/mass]]:''' 0.243&nbsp;hp/lb (0.399&nbsp;kW/kg)
 
== Lihat juga ==