A-4 Wanderer: Difference between revisions
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The [[A-4 Wanderer]] is a light scout [[:Category:Aircraft|aircraft]], capable of carrying one | [[Image:A-4.png|thumb|right|500px]] | ||
The [[A-4 Wanderer]] is a light scout [[:Category:Aircraft|aircraft]], capable of carrying one [[ARJ]] or small [[:Category:Vehicles|vehicle]].<br /> | |||
=== Statistics === | === Statistics === | ||
{{AirVehicle | |||
|manufacturer=[[:Category:Trimbal-Kneers Aerospace|Trimbal-Kneers Aerospace]] | |||
|role=Light scout aircraft | |||
|cargo_bays=1 | |||
|stowage=1 MT | |||
|weapon_mounts=2 | |||
|avionics_bays=2 | |||
|bypass_ratio=20% | |||
|critical_altitude=6 [[kilometer|km]] [[MSL]] | |||
|service_ceiling=22 [[kilometer|km]] [[MSL]] | |||
|max_speed=225 [[meter|m]]/s | |||
|fuel=9 MT | |||
|weight=17,158 kg | |||
|max_weight=41,067 kg (takeoff) | |||
|price=5,411,199 [[CR]] | |||
|vtol=Yes | |||
|rain_protection=None | |||
}} | |||
===Standard Equipment=== | ===Standard Equipment=== | ||
* [[GPWS]] | * [[GPWS]] | ||
* [[Autoflyte]] | * [[Autoflyte]] | ||
* 320 [[kilometer|km]] [[LRS]] with [[TCAS]] | * 320 [[kilometer|km]] [[LRS]] with [[TCAS]] | ||
== External Links == | == External Links == | ||
* [ | * [https://docs.google.com/spreadsheets/d/1LZlgMvasAq8s136n7vyUHRAif-GTyVNW9jFN70Lf7ug/edit?usp=sharing Detailed specifications] | ||
[[category:vehicles]] | [[category:vehicles]] | ||
[[category:aircraft]] | [[category:aircraft]] | ||
[[Category:Trimbal-Kneers Aerospace]] | [[Category:Trimbal-Kneers Aerospace]] | ||
Latest revision as of 16:15, 9 October 2026
The A-4 Wanderer is a light scout aircraft, capable of carrying one ARJ or small vehicle.
Statistics
| General | |||
|---|---|---|---|
| Manufacturer | Trimbal-Kneers Aerospace | Type / role | Light scout aircraft |
| Price / MSRP | 5,411,199 CR | Availability | Not specified |
| Restrictions | Not specified | IVR series | Not specified |
| Dimensions and weights | |||
| Length | Not specified | Width | Not specified |
| Height | Not specified | Empty / curb weight | 17,158 kg |
| Fuel capacity | 9 MT | Payload | Not specified |
| Maximum gross / takeoff weight | 41,067 kg (takeoff) | ||
| Capacity and equipment | |||
| Seats | Not specified | Passenger capacity | Not specified |
| Cargo bays | 1 | Cargo capacity | Not specified |
| Internal stowage | 1 MT | Avionics bays | 2 |
| Weapon mounts | 2 | Engine count | Not specified |
| Performance | |||
| Engine / propulsion | Not specified | Maximum speed | 225 m/s |
| Normal range | Not specified | Endurance | Not specified |
| Flight | |||
| Wingspan | Not specified | Effective wing area | Not specified |
| Cruising speed | Not specified | Service ceiling | 22 km MSL |
| Engine critical altitude | 6 km MSL | Bypass ratio | 20% |
| Thrust | Not specified | Maximum acceleration | Not specified |
| VTOL capability | Yes | Rain Protection Type | None |
| 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 |