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:''' ___
  
 
{{Craft
  
{{Craft
 
|name = LC-4
  
|name = LC-4
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}}
  
}}
 
}}
  
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==Development==
  +
  ⚫
==Design==
  +
  ⚫
==History==
  +
  ⚫
==Specifications (C512-100)==
  ⚫
'''General characteristics'''
  ⚫
*'''Crew:'''
  ⚫
** 4 pilots
  ⚫
** 320 passengers
  ⚫
*'''Capacity:''' ___,___ lb (___,___ kg)
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* '''Length:''' 185 ft 5 in (56.5 m)
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* '''Wingspan:''' 230 ft 4 in (56.5 m)
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* '''Height:''' 49 ft 3 in (15 m)
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* '''Wing area:''' ___
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*'''Empty weight:''' 352,078 lb (159,700 kg)
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  ⚫
*'''Powerplant:''' 6 × high bypass turbofan engines, 80,900 lbf (360 kN) thrust each
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'''Performance'''
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*'''Maximum speed:''' 402 mph (648 km/h, 350 kn)
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*'''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
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*'''Range:''' 1,000 km
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*'''Service ceiling:''' 41,000 ft (12,000 m)
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*'''Thrust/weight:''' ___

Revision as of 13:27, 23 May 2024

LC-4
Sloppmunjet LC-4 Monumentus
Strategic airlifter
Screenshot166.png
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)


Development

Design

History

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: 1,000 km
  • Service ceiling: 41,000 ft (12,000 m)
  • Thrust/weight: ___
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