Difference between revisions of "NEFA Laeno-76e"

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The '''NEFA Laeno-76e''' is a [[New Illyricum|New Illyrian]] [[Counter-insurgency aircraft]] produced by the [[Novo Elyreco Fareça Aviaçeona]] which is used by the [[New Illyrian Aviation Force]].
 
The '''NEFA Laeno-76e''' is a [[New Illyricum|New Illyrian]] [[Counter-insurgency aircraft]] produced by the [[Novo Elyreco Fareça Aviaçeona]] which is used by the [[New Illyrian Aviation Force]].
 
   
 
   
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==Specifications==
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{{Aircraft specs
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|prime units?=met
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<!--
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        General characteristics
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-->
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|crew=two
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|capacity=
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|length m=14.25
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|length ft=
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|length in=
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|length note=
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|span m=14.50
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|span ft=
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|span in=
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|span note=
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|height m=5.36
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|height ft=
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|height in=
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|height note=
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|wing area sqm=30.30
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|wing area sqft=
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|wing area note=
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|aspect ratio=6.9:1
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|airfoil=NACA 64<sub>2</sub>A215 at root, NACA64<sub>1</sub> at tip
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|empty weight kg=4020
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|empty weight lb=
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|empty weight note=
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|gross weight kg=
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|gross weight lb=
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|gross weight note=
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|max takeoff weight kg=6800
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|max takeoff weight lb=
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|max takeoff weight note=
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|fuel capacity={{convert|1280|L|abbr=on}} internal, up to {{convert|1736|L|abbr=on}} in external tanks
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|more general=
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<!--
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        Powerplant
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-->
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|eng1 number=2
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|eng1 name=[[Turbomeca Astazou]] XVIG
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|eng1 type=turboprop
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|eng1 kw=729<!-- prop engines -->
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|eng1 hp=<!-- prop engines -->
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|eng1 shp=<!-- prop engines -->
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|eng1 kn=<!-- jet/rocket engines -->
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|eng1 lbf=<!-- jet/rocket engines -->
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|eng1 note=
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|power original=
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|thrust original=
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|eng1 kn-ab=<!-- afterburners -->
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|eng1 lbf-ab=<!-- afterburners -->
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|prop blade number=<!-- propeller aircraft -->
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|prop name=
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|prop dia m=<!-- propeller aircraft -->
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|prop dia ft=<!-- propeller aircraft -->
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|prop dia in=<!-- propeller aircraft -->
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|prop dia note=
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<!--
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        Performance
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-->
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|max speed kmh=500
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|max speed mph=
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|max speed kts=
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|max speed note= at {{convert|3000|m|ft|-2|abbr=on}}
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|cruise speed kmh=430
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|cruise speed mph=
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|cruise speed kts=
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|cruise speed note=at {{convert|6000|ft|m|-2|abbr=on}} (econ cruise)
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|stall speed kmh=143
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|stall speed mph=
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|stall speed kts=
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|stall speed note=(flaps and undercarriage down)
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|never exceed speed kmh=750
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|never exceed speed mph=
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|never exceed speed kts=
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|never exceed speed note=
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|minimum control speed kmh=
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|minimum control speed mph=
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|minimum control speed kts=
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|minimum control speed note=
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|range km=
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|range miles=
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|range nmi=
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|range note=
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|combat range km=350
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|combat range miles=
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|combat range nmi=
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|combat range note=(Combat radius with {{convert|1500|kg|lb|-2|abbr=on}} weapons, High-low-high profile)
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|ferry range km=3710
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|ferry range miles=
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|ferry range nmi=
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|ferry range note=max internal and external fuel
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|endurance=<!-- if range unknown -->
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|ceiling m=10000
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|ceiling ft=
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|ceiling note=
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|g limits=+6/-3 g
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|roll rate=<!-- aerobatic -->
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|climb rate ms=18
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|climb rate ftmin=
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|climb rate note=
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|wing loading kg/m2=
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|wing loading lb/sqft=
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|wing loading note=
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|disk loading kg/m2=
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|disk loading lb/sqft=
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|disk loading note=
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|fuel consumption kg/km=
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|fuel consumption lb/mi=
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|power/mass=
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|thrust/weight=
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|more performance=
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<!--
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        Armament
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-->
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|guns= <br />
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**2× [[20 mm caliber|20 mm]] [[Ely-Pano]] HS.804 autocannons
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**4× [[7.62×51mm NATO|7.62 mm]] machine guns
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|bombs=
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|rockets= [[ARM-812-Marco]]
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|hardpoints=3
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|hardpoint capacity=centerline {{convert|1000|kg|lb|abbr=on}}, wing pylons {{convert|500|kg|lb|abbr=on}}, total external stores {{convert|1620|kg|lb|abbr=on}}
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|avionics=
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}}
 
{{New Illyricum topics}}
 
{{New Illyricum topics}}
 
[[Category:New Illyricum]]
 
[[Category:New Illyricum]]

Revision as of 10:20, 12 May 2024

NEFA Laeno-76e
Argentina Air Force FMA IA-58A Pucara (mod).jpg
NEFA Laeno-76e as part of the New Illyrian Aviation Force
Role
Counter-insurgency aircraft
National origin
 New Illyricum
Manufacturer
Novo Elyreco Fareça Aviaçeona
First flight
1970
Introduction
1975
Status
In Service
Primary user
New Illyrian Aviation Force

The NEFA Laeno-76e is a New Illyrian Counter-insurgency aircraft produced by the Novo Elyreco Fareça Aviaçeona which is used by the New Illyrian Aviation Force.

Specifications

General characteristics

  • Crew: two
  • Length: 14.25 m (46 ft 9 in)
  • Wingspan: 14.50 m (47 ft 7 in)
  • Height: 5.36 m (17 ft 7 in)
  • Wing area: 30.30 m2 (326.1 sq ft)
  • Aspect ratio: 6.9:1
  • Airfoil: NACA 642A215 at root, NACA641 at tip
  • Empty weight: 4,020 kg (8,863 lb)
  • Max takeoff weight: 6,800 kg (14,991 lb)
  • Fuel capacity: 1,280 L (280 imp gal; 340 US gal) internal, up to 1,736 L (382 imp gal; 459 US gal) in external tanks
  • Powerplant: 2 × Turbomeca Astazou XVIG turboprop, 729 kW (978 hp) each

Performance

  • Maximum speed: 500 km/h (310 mph, 270 kn) at 3,000 m (9,800 ft)
  • Cruise speed: 430 km/h (270 mph, 230 kn) at 6,000 ft (1,800 m) (econ cruise)
  • Stall speed: 143 km/h (89 mph, 77 kn) (flaps and undercarriage down)
  • Never exceed speed: 750 km/h (470 mph, 400 kn)
  • Combat range: 350 km (220 mi, 190 nmi) (Combat radius with 1,500 kg (3,300 lb) weapons, High-low-high profile)
  • Ferry range: 3,710 km (2,310 mi, 2,000 nmi) max internal and external fuel
  • Service ceiling: 10,000 m (33,000 ft)
  • g limits: +6/-3 g
  • Rate of climb: 18 m/s (3,500 ft/min)

Armament

  • Guns:
  • Hardpoints: 3 with a capacity of centerline 1,000 kg (2,200 lb), wing pylons 500 kg (1,100 lb), total external stores 1,620 kg (3,570 lb),
  • Rockets: ARM-812-Marco