R900 Trident: Difference between revisions
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|operators=Zephair<br>Sloppmunjet |
|operators=Zephair<br>Sloppmunjet |
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{{Craft/Aircraft |
{{Craft/Aircraft |
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| − | |mass=48, |
+ | |mass=48,918 kg |
|length=30.9 |
|length=30.9 |
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| − | |width= |
+ | |width=24.2 |
|height=9.2 |
|height=9.2 |
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|propulsion=2 turbofan engines and 1 centerline turbofan engine |
|propulsion=2 turbofan engines and 1 centerline turbofan engine |
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* '''Capacity:''' ___,___ lb (___,___ kg) |
* '''Capacity:''' ___,___ lb (___,___ kg) |
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* '''Length:''' 101 ft 5 in (30.9 m) |
* '''Length:''' 101 ft 5 in (30.9 m) |
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| − | * '''Wingspan:''' |
+ | * '''Wingspan:''' 79 ft 5 in (24.2 m) |
* '''Height:''' 30 ft 2 in (9.2 m) |
* '''Height:''' 30 ft 2 in (9.2 m) |
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| − | * '''Empty weight:''' 107,878 lb (48, |
+ | * '''Empty weight:''' 107,878 lb (48,918 kg) |
* '''Powerplant:''' 2 × Corain Motors PN-09-10 high bypass turbofan engines, 80,900 lbf (360 kN) thrust each |
* '''Powerplant:''' 2 × Corain Motors PN-09-10 high bypass turbofan engines, 80,900 lbf (360 kN) thrust each |
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Revision as of 01:11, 24 May 2024
|
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 |
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The Sloppmunjet R900 Trident is a 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: 107,878 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: ___