W-6 Manx: Difference between revisions
From Rise: The Vieneo Province
(→Standard Equipment: Add flap detents, controls and VMU confirmations) |
(Document code-backed cabin pressurization and differential-pressure rating) |
||
| Line 6: | Line 6: | ||
== Statistics == | == Statistics == | ||
{{AerospaceVehicle | {{AerospaceVehicle | ||
|cabin_pressurization=Pressurized — stored breathing gas | |||
|max_pressure_diff=2,400 mbar (240 kPa), cabin above surroundings | |||
|manufacturer=[[:Category:Trimbal-Kneers Aerospace|Trimbal-Kneers Aerospace]] | |manufacturer=[[:Category:Trimbal-Kneers Aerospace|Trimbal-Kneers Aerospace]] | ||
|role=Aerospace vehicle | |role=Aerospace vehicle | ||
Revision as of 13:33, 1 November 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 |
| Life support | |||
| Cabin pressurization | Pressurized — stored breathing gas | Rated pressure differential | 2,400 mbar (240 kPa), cabin above surroundings |
| 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 |
| Touchdown descent design limit | Not specified | Crosswind component limit | Not established |
| 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 | ||
Standard Equipment
- GPWS
- VMU engine-failure warnings and flap-position confirmations.
- Trailing-edge flap detents at 0°, 8°, 20°, 30° and 40°. The default bindings are Shift+F8 to extend one detent and Shift+F9 to retract one detent; custom bindings may differ. The VMU confirms the selected detent when the flaps reach it, in either direction.
- Autoflyte
- VTOL
- 320 km LRS with TCAS