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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| − | The '''Sloppmunjet R900 Trident''' is a narrow-body trijet airliner designed and produced by [[Sloppmunjet]] in [[Ikonia]]. |
+ | The '''Sloppmunjet R900 Trident''' is a supersonic narrow-body trijet airliner designed and produced by [[Sloppmunjet]] in [[Ikonia]]. |
== Development == |
== Development == |
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== Design == |
== Design == |
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| + | 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. |
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== History == |
== History == |
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== Variants == |
== Variants == |
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| − | == Specifications == |
+ | == Specifications (R900 Trident) == |
| + | '''General characteristics''' |
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| + | |||
| + | * '''Crew:''' |
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| + | ** 2 pilots |
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| + | ** 32 passengers |
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| + | * '''Capacity:''' ___,___ lb (___,___ kg) |
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| + | * '''Length:''' 101 ft 5 in (30.9 m) |
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| + | * '''Wingspan:''' 79 ft 5 in (24.2 m) |
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| + | * '''Height:''' 30 ft 2 in (9.2 m) |
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| + | * '''Empty weight:''' 107,846 lb (48,918 kg) |
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| + | |||
| + | * '''Powerplant:''' 2 × 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:''' 1,007 mph (1,620 km/h, 875 kn) |
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| + | * '''Maximum speed:''' Mach 1.4 (at 6,000 m, 20,000 ft) |
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| + | * '''Cruise speed:''' 738 mph (1,188 km/h, 641 kn) / Mach 1.2 |
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| + | * '''Range:''' 2,000 km |
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| + | * '''Service ceiling:''' 41,000 ft (12,000 m) |
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| + | * '''Thrust/weight:''' ___ |
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[[Category:Aircraft]] |
[[Category:Aircraft]] |
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Latest revision as of 18:16, 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 |
||||
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: ___