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At a glance
Measured figures
Empty; C-47B-DK · Empty weight
Single sourceGross; C-47B-DK · Gross weight
Single sourceMaximum take-off; C-47B-DK · Max takeoff weight
Single source18,135 lb (8,226 kg)[source]
26,000 lb (11,793 kg)[source]
31,000 lb (14,061 kg)[source]
Maximum take-off; Max takeoff weight
Single source45,246 kg (99,750 lb)[source]
Cruise; C-47B-DK · Cruise speed
Single sourceMaximum; C-47B-DK · at 10,000 ft (3,000 m)
Single source224 mph (360 km/h, 195 kn) at 10,000 ft (3,000 m)[source]
160 mph (260 km/h, 140 kn)[source]
Cruise; (0.85 Mach at a cruise altitude of 41,000 ft (12,000 m))
Single sourceMaximum; (0.89 Mach at a cruise altitude of 41,000 ft (12,000 m))
Single sourceMaximum; Maximum speed
Single source946 km/h (588 mph, 511 kn) (0.89 Mach at a cruise altitude of 41,000 ft (12,000 m))[source]
904 km/h (562 mph, 488 kn) (0.85 Mach at a cruise altitude of 41,000 ft (12,000 m))[source]
Maximum speed: 946 km/h (588 mph, 511 kn)[source]Hensoldt Pegasus · Specifications · Maximum speed: 946 km/h (588 mph, 511 kn) (0.89 Mach at a cruise altitude of 41,000 ft (12,000 m))
C-47B-DK · 2 × Pratt & Whitney R-1830-90C Twin Wasp 14-cylinder air-cooled radial piston engines takeoff rating
Single sourceC-47B-DK · normal rating at 14,500 ft (4,400 m)
Single source2 × Pratt & Whitney R-1830-90C Twin Wasp 14-cylinder air-cooled radial piston engines 1,200 hp (890 kW) takeoff rating 1,000 hp (750 kW) normal rating at 14,500 ft (4,400 m)[source]
2 × BR700-710A2-20 turbofan thrust each
Single source2 × BR700-710A2-20 turbofan , 65.6 kN (14,700 lbf) thrust each[source]
C-47B-DK · Wing area
Single source987 sq ft (91.7 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Douglas C-47 Skytrain | Hensoldt Pegasus |
|---|---|---|
| Type | Military transport aircraft[source] | — |
| National origin | United States[source] | Germany Canada United States[source] |
| Manufacturer | Douglas Aircraft Company[source] | General contractor : Hensoldt Sub-contractors / systems supplies : Hensoldt Bombardier Aviation Bombardier Defense Lufthansa Technik Defense[source] |
| Status | In service[source] | — |
| Primary users | United States Army Air Forces Royal Air Force United States Navy Royal Canadian Air Force See operators[source] | — |
| Number built | 10,174[source] | 3 (being manufactured)[source] |
| First flight | 23 December 1941 ( 1941-12-23 )[source] | — |
| Developed from | Douglas DC-3[source] | Global 6000[source] |
| Variants | Douglas XCG-17 Douglas AC-47 Spooky Douglas R4D-8[source] | — |
| Capacity | 28 troops or 6,000 lb (2,700 kg) of cargo[source] | — |
| Airfoil | root: NACA 2215 ; tip: NACA 2206[source] | — |
| Propellers | 3-bladed constant-speed propellers[source] | — |
| Time to altitude | 10,000 ft (3,000 m) in 9 minutes 30 seconds[source] | — |
| Wing loading | 26.3 lb/sq ft (128 kg/m 2 )[source] | — |
| Power/mass | 0.0926 hp/lb (0.1522 kW/kg)[source] | — |
| Role | — | SIGINT and reconnaissance[source] |
| Service | — | German Air Force[source] |
| Manufactured | — | Since 2022[source] |
| Introduction date | — | Planned for 2027[source] |
| Initiated | — | June 2021.[source] |
| Fuel capacity | — | 20.43 t (45,000 lb)[source] |
| Cabin height | — | 1.88 m (6.2 ft)[source] |
| Cabin width | — | 2.41 m (7.9 ft)[source] |
| Cabin length | — | 14.80 m (48.6 ft)[source] |
| Flight avionic | — | Bombardier Vision (four large displays, a head-up display, an enhanced vision system and synthetic vision system, graphic flight planning and multiscan weather radar)[source] |
| Radar and radio electronic signal collection and analysis | — | Hensoldt Kalætron Integral (30MHz to 40GHz)[source] |
| Source measurement | — | The origins of the Pegasus can be traced back to the decommissioning of the German Navy 's Breguet 1150 M Atlantic in 2010, which left a long-lasting capability gap in the Bundeswehr in the area of signal-detecting airborne long-range surveillance and reconnaissance capability. During the late 2000s and early 2010s, work was undertaken on developing the RQ-4 Global Hawk unmanned aerial vehicle (UAV) into a specialised variant, known as EuroHawk , that was originally intended as the delivery system for this capability. However, the EuroHawk was reportedly not capable of being certifiable under ICAO rules without an anti-collision system; thus preventing any operations within European airspace or the airspace of any ICAO member; accordingly, on 15 May 2013, the German government announced the immediate termination of the Eurohawk program.[source]Hensoldt Pegasus · Development / Background; only the objects and conditions stated in this passage Length: 30.30 m (99 ft 5 in)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Wingspan: 28.70 m (94 ft 2 in)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Height: 7.80 m (25 ft 7 in)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Max takeoff weight: 45,246 kg (99,750 lb)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Fuel capacity: 20.43 t (45,000 lb)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Cabin height : 1.88 m (6.2 ft)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Cabin width : 2.41 m (7.9 ft)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Cabin length : 14.80 m (48.6 ft)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Powerplant: 2 × BR700-710A2-20 turbofan , 65.6 kN (14,700 lbf) thrust each[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Maximum speed: 946 km/h (588 mph, 511 kn) (0.89 Mach at a cruise altitude of 41,000 ft (12,000 m))[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Cruise speed: 904 km/h (562 mph, 488 kn) (0.85 Mach at a cruise altitude of 41,000 ft (12,000 m))[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Range: 6,000 km (3,700 mi, 3,200 nmi)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Service ceiling: 16,000 m (51,000 ft)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage Radar and radio electronic signal collection and analysis: Hensoldt Kalætron Integral (30MHz to 40GHz)[source]Hensoldt Pegasus · Specifications; only the objects and conditions stated in this passage |
| Reported operators |
| — |