R900 Trident

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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 48,918 kg
Length 30.9 m
Width 24.2 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 supersonic narrow-body trijet airliner designed and produced by Sloppmunjet in Ikonia.

Development

Design

History

Variants

Specifications (R900 Trident)

General characteristics

  • Crew:
    • 2 pilots
    • 32 passengers
  • Capacity: ___,___ lb (___,___ kg)
  • Length: 101 ft 5 in (30.9 m)
  • Wingspan: 79 ft 5 in (24.2 m)
  • Height: 30 ft 2 in (9.2 m)
  • Empty weight: 107,846 lb (48,918 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: ___