W-6 Manx: Difference between revisions
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[[Image: | [[Image:Hanger_Manx.png|thumb|right|900px]] | ||
== W-6 Manx Class == | == W-6 Manx Class == | ||
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== Statistics == | == Statistics == | ||
= | {{AerospaceVehicle | ||
|manufacturer=[[:Category:Trimbal-Kneers Aerospace|Trimbal-Kneers Aerospace]] | |||
|role=Aerospace vehicle | |||
|max_speed=94 [[meter|m]]/s IAS at [[MSL]] | |||
|cruise_speed=539 [[meter|m]]/s at 15 [[kilometer|km]] | |||
|service_ceiling=Indefinite (capable of reaching [[escape velocity]]) | |||
|range=Indefinite (capable of reaching [[orbit]]) | |||
|thrust=1,029,817 N | |||
|weapon_mounts=1 | |||
|engines=2 | |||
|cargo_bays=3 | |||
|avionics_bays=4 | |||
|stowage=7 MT (Bay 0), or 6 passengers | |||
|passengers=6 in Bay 0 instead of cargo | |||
|acceleration=About 1 G fully loaded and fueled; depends on weight | |||
|price=3,989,373 [[CR]] | |||
|wingspan=50.1 [[meter|m]] | |||
|length=44.9 [[meter|m]] | |||
|height=9.4 [[meter|m]] (with gear) | |||
|wing_area=588 m<sup>2</sup> | |||
|weight=50,000 kg ([[BOW]]) | |||
|fuel=12,000 kg ([[Iagreous]]) | |||
|payload=43,009 kg | |||
|max_weight=105,009 kg (gross) | |||
|vtol=Limited | |||
|orbital_capability=Capable of reaching [[orbit]] and [[escape velocity]] | |||
}} | |||
===Standard Equipment=== | ===Standard Equipment=== | ||
Latest revision as of 16:06, 9 October 2026
W-6 Manx Class
The W-6 is a limited-VTOL-capable aerospace vehicle, in so far as it has conventional flight surfaces but is also capable of ascending beyond the atmosphere, maneuvering in orbit and re-entering under its own power.
Statistics
| General | |||
|---|---|---|---|
| Manufacturer | Trimbal-Kneers Aerospace | Type / role | Aerospace vehicle |
| Price / MSRP | 3,989,373 CR | Availability | Not specified |
| Restrictions | Not specified | IVR series | Not specified |
| Dimensions and weights | |||
| Length | 44.9 m | Width | Not specified |
| Height | 9.4 m (with gear) | Empty / curb weight | 50,000 kg (BOW) |
| Fuel capacity | 12,000 kg (Iagreous) | Payload | 43,009 kg |
| Maximum gross / takeoff weight | 105,009 kg (gross) | ||
| Capacity and equipment | |||
| Seats | Not specified | Passenger capacity | 6 in Bay 0 instead of cargo |
| Cargo bays | 3 | Cargo capacity | Not specified |
| Internal stowage | 7 MT (Bay 0), or 6 passengers | Avionics bays | 4 |
| Weapon mounts | 1 | Engine count | 2 |
| Performance | |||
| Engine / propulsion | Not specified | Maximum speed | 94 m/s IAS at MSL |
| Normal range | Indefinite (capable of reaching orbit) | Endurance | Not specified |
| Flight | |||
| Wingspan | 50.1 m | Effective wing area | 588 m2 |
| Cruising speed | 539 m/s at 15 km | Service ceiling | Indefinite (capable of reaching escape velocity) |
| Engine critical altitude | Not specified | Bypass ratio | Not specified |
| Thrust | 1,029,817 N | Maximum acceleration | About 1 G fully loaded and fueled; depends on weight |
| VTOL capability | Limited | Rain Protection Type | Bleed air system |
| Flight controls and landing gear | |||
| Flight Spoilers | Not specified | Ground Lift Dump (GLD) | Not specified |
| Retractable Landing Gear | Not specified | Landing Gear Type | Not specified |
| Leading Edge Flaps | Not specified | Trailing Edge Flaps | Not specified |
| Space operations | |||
| Orbital capability | Capable of reaching orbit and escape velocity | Interstellar capability | Not specified |
| Docking / interfaces | Not specified | ||