R900 Trident
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R900
Sloppmunjet R900 Trident
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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 |
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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
The trijet configuration and in-line engine placement of the R900 enables it to reach very high speeds. This makes it popular amongst business passengers. However, the greater discomfort associated with supersonic travel deters long-haul flyers.
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: ___