LC-4 Monumentus: Difference between revisions
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|operators=[[Ikonic Air Force]] |
|operators=[[Ikonic Air Force]] |
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{{Craft/Aircraft |
{{Craft/Aircraft |
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− | |mass= |
+ | |mass=160,088 kg |
− | |length= |
+ | |length=55.8 |
− | |width= 70. |
+ | |width= 70.7 |
− | |height= |
+ | |height=17.4 |
|propulsion=6 x High Bypass Turbofan Engines |
|propulsion=6 x High Bypass Turbofan Engines |
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|speed=180 m/s |
|speed=180 m/s |
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− | |range= |
+ | |range=2,000 |
|crew=4 |
|crew=4 |
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|variants=LC-4 (2 built) |
|variants=LC-4 (2 built) |
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*'''Maximum speed:''' Mach 0.57 (at 6,000 m, 20,000 ft) |
*'''Maximum speed:''' Mach 0.57 (at 6,000 m, 20,000 ft) |
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*'''Cruise speed:''' 390 mph (627 km/h, 339 kn) / Mach 0.55 |
*'''Cruise speed:''' 390 mph (627 km/h, 339 kn) / Mach 0.55 |
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− | *'''Range:''' |
+ | *'''Range:''' 2,000 km |
*'''Service ceiling:''' 41,000 ft (12,000 m) |
*'''Service ceiling:''' 41,000 ft (12,000 m) |
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*'''Thrust/weight:''' ___ |
*'''Thrust/weight:''' ___ |
Revision as of 02:13, 24 May 2024
LC-4
Sloppmunjet LC-4 Monumentus
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Strategic airlifter | |||||
LC-4-001 'Deus Fortima' of the Ikonic Air Force during a flight to Bastion Proving Grounds. | |||||
National Origin | Ikonia | ||||
Production History | |||||
Produced | |||||
2181 - 2189 | |||||
Designer | Sloppmunjet | ||||
Number Built | 2 | ||||
Service History | |||||
In Service | |||||
2185 - Ongoing | |||||
Used By | Ikonic Air Force | ||||
Aircraft Characteristics | |||||
Dry Mass | 160,088 kg | ||||
Length | 55.8 m | ||||
Width | 70.7 m | ||||
Height | 17.4 m | ||||
Propulsion | 6 x High Bypass Turbofan Engines | ||||
Maximum Velocity | 180 m/s | ||||
Operational Range | 2,000 km | ||||
Crew | 4 | ||||
Variants | LC-4 (2 built) |
The Sloppmunjet LC-4 Monumentus is a strategic heavy lift cargo aircraft designed and produced by Sloppmunjet in Ikonia.
Development
Design
History
Accidents and Incidents
Specifications (C512-100)
General characteristics
- Crew:
- 4 pilots
- 320 passengers
- Capacity: ___,___ lb (___,___ kg)
- Length: 185 ft 5 in (56.5 m)
- Wingspan: 230 ft 4 in (56.5 m)
- Height: 49 ft 3 in (15 m)
- Wing area: ___
- Empty weight: 352,078 lb (159,700 kg)
- Powerplant: 6 × high bypass turbofan engines, 80,900 lbf (360 kN) thrust each
Performance
- Maximum speed: 402 mph (648 km/h, 350 kn)
- Maximum speed: Mach 0.57 (at 6,000 m, 20,000 ft)
- Cruise speed: 390 mph (627 km/h, 339 kn) / Mach 0.55
- Range: 2,000 km
- Service ceiling: 41,000 ft (12,000 m)
- Thrust/weight: ___