Difference between revisions of "Aermachina AC-32"
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==Specifications== | ==Specifications== | ||
| + | |||
| + | {{Aircraft specs | ||
| + | |ref=<!-- reference --> | ||
| + | |prime units?=kts | ||
| + | <!-- | ||
| + | General characteristics | ||
| + | --> | ||
| + | |genhide= | ||
| + | |||
| + | |crew= One pilot | ||
| + | |capacity= | ||
| + | |length m= | ||
| + | |length ft= 52 | ||
| + | |length in= | ||
| + | |span m= | ||
| + | |span ft= 36 | ||
| + | |span in= | ||
| + | |height m= | ||
| + | |height ft= 20 | ||
| + | |height in= | ||
| + | |wing area sqm= | ||
| + | |wing area sqft= | ||
| + | |wing area note= | ||
| + | |airfoil= | ||
| + | |empty weight kg= | ||
| + | |empty weight lb= 24500 | ||
| + | |empty weight note= | ||
| + | |gross weight kg= | ||
| + | |gross weight lb= 35500 | ||
| + | |gross weight note= | ||
| + | |fuel capacity= | ||
| + | |more general= | ||
| + | <!-- | ||
| + | Powerplant | ||
| + | --> | ||
| + | |eng1 number= 1 | ||
| + | |eng1 name= [[Elettrico Nazionale F100]] | ||
| + | |eng1 type= afterburning turbofan | ||
| + | |eng1 lbf= 14600 | ||
| + | |eng1 lbf-ab= 23700 | ||
| + | |more power= | ||
| + | <!-- | ||
| + | Performance | ||
| + | --> | ||
| + | |perfhide= | ||
| + | |||
| + | |max speed kmh= | ||
| + | |max speed mph= | ||
| + | |max speed kts= | ||
| + | |max speed mach= 2 | ||
| + | |cruise speed kts= | ||
| + | |never exceed speed kts= | ||
| + | |range nmi= | ||
| + | |combat range nmi= 700 | ||
| + | |endurance=<!-- if range unknown --> | ||
| + | |ceiling m= | ||
| + | |ceiling ft= 50000 | ||
| + | |g limits= +9.0 | ||
| + | |roll rate=<!-- aerobatic --> | ||
| + | |climb rate ms= | ||
| + | |climb rate ftmin= | ||
| + | |lift to drag= | ||
| + | |wing loading kg/m2= | ||
| + | |wing loading lb/sqft= | ||
| + | |wing loading note= | ||
| + | |more performance= | ||
| + | <!-- | ||
| + | Armament | ||
| + | --> | ||
| + | |armament=<!-- add bulletted list here or if you want to use the following | ||
| + | specific parameters, remove this parameter--> | ||
| + | |guns= | ||
| + | |bombs= | ||
| + | |rockets= | ||
| + | |missiles= | ||
| + | |hardpoints= | ||
| + | |hardpoint capacity= | ||
| + | |hardpoint rockets= | ||
| + | |hardpoint missiles= | ||
| + | |hardpoint bombs= | ||
| + | |hardpoint other= | ||
| + | |||
| + | |avionics= | ||
| + | }} | ||
==See also== | ==See also== | ||
[[Category:Salisford]] | [[Category:Salisford]] | ||
| + | [[Category:Aircraft]] | ||
Latest revision as of 14:41, 16 August 2022
| Aermachina AC-32 | |
|---|---|
| |
| Scale model of the AC-32 undergoing aerodynamic testing. | |
Role
|
Multirole fighter, air superiority fighter |
National origin
|
Salisford |
Manufacturer
|
Aermachina |
First flight
|
27 March 1980 |
Introduction
|
6 June 1981 |
Status
|
In service |
Produced
|
1980–present |
Number built
|
432 |
The Aermachina AC-32 is a single-engine multi-role fighter aircraft developed by Aermachina for the Royal Salisfordian Air Force. Originally designed as an air superiority fighter, it eventually evolved into a all-weather multi-role aircraft. Over 400 have been built since production was approved in 1978.
The AC-32 is the workhorse of the Royal Salisfordian Air Force, and makes up the majority of Salisford's air superiority and ground attack capabilities.
Contents
Development
Design
Operational History
Variants
Operators
Specifications
General characteristics
- Crew: One pilot
- Length: 52 ft (16 m)
- Wingspan: 36 ft (11 m)
- Height: 20 ft (6.1 m)
- Empty weight: 24,500 lb (11,113 kg)
- Gross weight: 35,500 lb (16,103 kg)
- Powerplant: 1 × Elettrico Nazionale F100 afterburning turbofan, 14,600 lbf (65 kN) thrust dry, 23,700 lbf (105 kN) with afterburner
Performance
- Maximum speed: Mach 2
- Combat range: 700 nmi (810 mi, 1,300 km)
- Service ceiling: 50,000 ft (15,000 m)
- g limits: +9.0
