R900 Trident

R900 Sloppmunjet R900 Trident
Narrow-body airliner
National Origin		Ikonia
Production History
Produced
2179 - Ongoing
Designer		Sloppmunjet
Unit Cost		47,806(√)
Number Built		76
Service History
Used By		Zephair Sloppmunjet
Aircraft Characteristics
Dry Mass		48,933 kg
Length		30.9 m
Width		25.3 m
Height		9.2 m
Propulsion		2 turbofan engines and 1 centerline turbofan engine
Maximum Velocity		450 m/s
Operational Range		2,000 km
Crew		2 pilots 32 passengers
Variants		Sloppmunjet R900 Trident Sloppmunjet R900 Demeter

The Sloppmunjet R900 Trident is a narrow-body trijet airliner designed and produced by Sloppmunjet in Ikonia.

Specifications (R900 Trident)

General characteristics

• Crew:
  • 2 pilots
  • 32 passengers
• Capacity: ___,___ lb (___,___ kg)
• Length: 101 ft 5 in (30.9 m)
• Wingspan: 86 ft 1 in (25.3 m)
• Height: 30 ft 2 in (9.2 m)
• Empty weight: 107,878 lb (48,933 kg)

• Powerplant: 2 × Corain Motors PN-09-10 high bypass turbofan engines, 80,900 lbf (360 kN) thrust each

Performance

• Maximum speed: 1,007 mph (1,620 km/h, 875 kn)
• Maximum speed: Mach 1.4 (at 6,000 m, 20,000 ft)
• Cruise speed: 738 mph (1,188 km/h, 641 kn) / Mach 1.2
• Range: 2,000 km
• Service ceiling: 41,000 ft (12,000 m)
• Thrust/weight: ___