LC-4 Monumentus: Difference between revisions
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+ | == Development == |
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+ | |||
+ | == Design == |
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+ | |||
+ | == History == |
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+ | |||
+ | ==Specifications (C512-100)== |
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+ | '''General characteristics''' |
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+ | *'''Crew:''' |
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+ | **2 pilots |
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+ | **240 passengers |
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+ | *'''Capacity:''' ___,___ lb (___,___ kg) |
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+ | *'''Length:''' 202 ft 5 in (61.7 m) |
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+ | *'''Wingspan:''' 162 ft 1 in (49.4 m) |
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+ | *'''Height:''' 56 ft 1 in (17.1 m) |
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+ | *'''Wing area:''' ___ |
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+ | *'''Empty weight:''' 364,942 lb (165,535 kg) |
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+ | |||
+ | *'''Powerplant:''' 6 × Corain Motors PN-09-10 high bypass turbofan engines, 80,900 lbf (360 kN) thrust each |
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+ | '''Performance''' |
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+ | *'''Maximum speed:''' 492 mph (792 km/h, 428 kn) |
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+ | *'''Maximum speed:''' Mach 0.7 (at 6,000 m, 20,000 ft) |
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+ | *'''Cruise speed:''' 450 mph (724 km/h, 391 kn) / Mach 0.64 |
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+ | *'''Range:''' 400 km |
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+ | *'''Service ceiling:''' 41,000 ft (12,000 m) |
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+ | *'''Thrust/weight:''' ___ |
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{{Craft |
{{Craft |
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|name = LC-4 |
|name = LC-4 |
Revision as of 12:19, 23 May 2024
Development
Design
History
Specifications (C512-100)
General characteristics
- Crew:
- 2 pilots
- 240 passengers
- Capacity: ___,___ lb (___,___ kg)
- Length: 202 ft 5 in (61.7 m)
- Wingspan: 162 ft 1 in (49.4 m)
- Height: 56 ft 1 in (17.1 m)
- Wing area: ___
- Empty weight: 364,942 lb (165,535 kg)
- Powerplant: 6 × Corain Motors PN-09-10 high bypass turbofan engines, 80,900 lbf (360 kN) thrust each
Performance
- Maximum speed: 492 mph (792 km/h, 428 kn)
- Maximum speed: Mach 0.7 (at 6,000 m, 20,000 ft)
- Cruise speed: 450 mph (724 km/h, 391 kn) / Mach 0.64
- Range: 400 km
- Service ceiling: 41,000 ft (12,000 m)
- Thrust/weight: ___
LC-4
Sloppmunjet LC-4 Monumentus
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Strategic airlifter | |||||
Ikonic Air Force LC-4 during a routine flight. | |||||
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 | 159,700 kg | ||||
Length | 56.5 m | ||||
Width | 70.2 m | ||||
Height | 15 m | ||||
Propulsion | 6 x High Bypass Turbofan Engines | ||||
Maximum Velocity | 180 m/s | ||||
Operational Range | 1,000 km | ||||
Crew | 4 | ||||
Variants | LC-4 (2 built) |