Aetherdyne Ae-15 Ayame (Pacifica): Difference between revisions

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Tag: 2017 source edit
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==Design==
==Design==
===Overview===
===Overview===
The Ae-15 was designed as a large multirole air superiority and strike fighter using a conventional wing-tailplane layout, hybrid semi-monocoque construction using metal and composite materials, a one-seat or two-seat cockpit supporting either a pilot or a pilot and a WSO, two afterburning turbofan engines, an AESA radar array, and low-observable construction techniques.
<br>Features such as the engines, airframe, and avionics are greatly improved over previous Pelinese aircraft designs due to better access to tooling, expertise, and technology; subsequent upgrades in the form of the Ae-15B and Ae-15V variants have brought further increases in the sophistication of avionics systems in particular.
===Airframe===
===Airframe===
The Ae-15 has an angular fuselage with forward-swept, side-mounted air intakes, a conventional wing-tailplane layout of [[Wikipedia:Delta wing|delta wings]] incorporating [[Wikipedia:Leading-edge extension#Leading-edge root extension|leading-edge root extensions]] and [[Wikipedia:Chine|chines]], and [[Wikipedia:Twin tail|twin]] outwards-canted [[Wikipedia:Vertical stabilizer|vertical stabilizers]].
The Ae-15 has an angular semi-monocoque fuselage with forward-swept, side-mounted air intakes, a conventional wing-tailplane layout of shoulder-mounted [[Wikipedia:Delta wing|delta wings]] incorporating [[Wikipedia:Leading-edge extension#Leading-edge root extension|leading-edge root extensions]] and [[Wikipedia:Chine|chines]], and [[Wikipedia:Twin tail|twin]] outwards-canted [[Wikipedia:Vertical stabilizer|vertical stabilizers]]. [[Wikipedia:Stabilator|elevons]] are used for the tailplane in order to reduce mass. The aerodynamic characteristics of the Ae-15 are [[Wikipedia:Relaxed stability#Intentional instability|intentionally unstable]] in order to improve maneuverability for within-visual-range engagements against contemporary fighter aircraft.
<br>The structure of the Ae-15 incorporates features such as radar-absorbent paint, [[Wikipedia:S-duct|S-ducts]] in front of the engine compressors, and sawtoothed panel joints to reduce [[Wikipedia:Radar cross section|radar cross section]]. Modern aerospace manufacturing materials such as [[Wikipedia:Fibre-reinforced plastic|fiber-reinforced polymers]] and [[Wikipedia:Aluminium-scandium alloy|aluminium-scandium alloy]] are also used extensively and to a much greater degree than preceding Pelinese fighter aircraft such as the Ae-13, allowing for a higher payload capacity and greater combat range. The canopy of the Ae-15 is [[Wikipedia:Bubble canopy|frameless]] and coated in a layer of [[Wikipedia:Indium tin oxide|indium tin oxide]] to prevent radar returns from internal features of the aircraft’s cockpit.
<br>The structure of the Ae-15 incorporates features such as radar-absorbent paint, [[Wikipedia:S-duct|S-ducts]] in front of the engine compressors, and sawtoothed panel joints to reduce [[Wikipedia:Radar cross section|radar cross section]]. Modern aerospace manufacturing materials such as [[Wikipedia:Fibre-reinforced plastic|fiber-reinforced polymers]] and [[Wikipedia:Aluminium-scandium alloy|aluminium-scandium alloy]] are also used extensively and to a much greater degree than preceding Pelinese fighter aircraft such as the Ae-13, allowing for a higher payload capacity and greater combat range. The canopy of the Ae-15 is [[Wikipedia:Bubble canopy|frameless]] and is coated in a layer of [[Wikipedia:Indium tin oxide|indium tin oxide]] in order to prevent radar returns from internal features of the aircraft’s cockpit.
 
===Armament===
===Armament===
===Avionics===
===Avionics===
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|eng1 name = Yuzimashi AF-11D
|eng1 name = Yuzimashi AF-11D
|eng1 type = [[Wikipedia:Afterburner|afterburning]] [[Wikipedia:Turbofan#Low-bypass turbofan|low-bypass turbofan]] engines
|eng1 type = [[Wikipedia:Afterburner|afterburning]] [[Wikipedia:Turbofan#Low-bypass turbofan|low-bypass turbofan]] engines
|eng1 kn = 100
|eng1 kn = 130
|eng1 kn-ab = 150
|eng1 kn-ab = 180


|max speed kmh = 2,600
|max speed kmh = 2,600
Line 72: Line 73:
|climb rate ms = 300
|climb rate ms = 300
|wing loading kg/m2 = 406.7
|wing loading kg/m2 = 406.7
|thrust/weight = 1.05
|thrust/weight = 1.27


|guns = 1 x 30mm autocannon with up to 200 rounds
|guns = 1 x 30mm autocannon with up to 200 rounds
|hardpoints = 8 external hardpoints
|hardpoints = 4 external hardpoints
|hardpoint capacity = 6,000kg
|hardpoint capacity = 8,000kg
|hardpoint missiles = {{bulleted list
|hardpoint missiles = {{bulleted list
|N06A Ruby short range [[Wikipedia:Air-to-air missile|AAM]]
|N06A Ruby short range [[Wikipedia:Air-to-air missile|AAM]]

Revision as of 15:57, 1 September 2023

Ae-15 Ayame
Role Strike fighter
National origin  Pelinai
Manufacturer Aetherdyne IDB
First flight February 7, 2005
Introduction October 19, 2008
Status In service
Primary user Pelinai (Pacifica)Royal Pelinese Air Force
Produced 2005–present
Number built Ae-15A/B/V/S/U: approx. 1600+ (as of 2023)

The Aetherdyne Ae-15 Ayame (Pelinese: イシ-15 あやめ, Ishi-15 Ayame) is a Pelinese twin-engine, all-weather, low-observable strike fighter aircraft developed and manufactured by Aetherdyne. Variants of the Ae-15 are the current principal air superiority and strike fighter aircraft of the Royal Pelinese Air Force, with over 1,600 serial production versions built since 2008.

The Ae-15 made its maiden flight on February 7, 2005, and was accepted into RPAF service on November 2, 2008; its intended combat roles include air superiority, interdiction, and close air support.

Development

Design

Overview

The Ae-15 was designed as a large multirole air superiority and strike fighter using a conventional wing-tailplane layout, hybrid semi-monocoque construction using metal and composite materials, a one-seat or two-seat cockpit supporting either a pilot or a pilot and a WSO, two afterburning turbofan engines, an AESA radar array, and low-observable construction techniques.
Features such as the engines, airframe, and avionics are greatly improved over previous Pelinese aircraft designs due to better access to tooling, expertise, and technology; subsequent upgrades in the form of the Ae-15B and Ae-15V variants have brought further increases in the sophistication of avionics systems in particular.

Airframe

The Ae-15 has an angular semi-monocoque fuselage with forward-swept, side-mounted air intakes, a conventional wing-tailplane layout of shoulder-mounted delta wings incorporating leading-edge root extensions and chines, and twin outwards-canted vertical stabilizers. elevons are used for the tailplane in order to reduce mass. The aerodynamic characteristics of the Ae-15 are intentionally unstable in order to improve maneuverability for within-visual-range engagements against contemporary fighter aircraft.
The structure of the Ae-15 incorporates features such as radar-absorbent paint, S-ducts in front of the engine compressors, and sawtoothed panel joints to reduce radar cross section. Modern aerospace manufacturing materials such as fiber-reinforced polymers and aluminium-scandium alloy are also used extensively and to a much greater degree than preceding Pelinese fighter aircraft such as the Ae-13, allowing for a higher payload capacity and greater combat range. The canopy of the Ae-15 is frameless and is coated in a layer of indium tin oxide in order to prevent radar returns from internal features of the aircraft’s cockpit.

Armament

Avionics

Engines

Upgrades

Variants

Production models

Research aircraft

Operators

 Kingdom of Pelinai

Specifications (Ae-15V)

General characteristics

  • Crew: one (pilot)
  • Length: 22.4 m (73 ft 6 in)
  • Wingspan: 13.0 m (42 ft 8 in)
  • Height: 4.5 m (14 ft 9 in)
  • Wing area: 71.3 m2 (767 sq ft)
  • Empty weight: 19,000 kg (41,888 lb)
  • Gross weight: 29,000 kg (63,934 lb)
  • Max takeoff weight: 40,000 kg (88,185 lb)
  • Fuel capacity: roughly 13,000kg internally
  • Powerplant: 2 × Yuzimashi AF-11D afterburning low-bypass turbofan engines, 130 kN (29,000 lbf) thrust each dry, 180 kN (40,000 lbf) with afterburner

Performance

  • Maximum speed: 2,600 km/h (1,600 mph, 1,400 kn)
  • Maximum speed: Mach 2.1
  • Cruise speed: 2,200 km/h (1,400 mph, 1,200 kn)
  • Range: 6,000 km (3,700 mi, 3,200 nmi)
  • Combat range: 2,000 km (1,200 mi, 1,100 nmi)
  • Service ceiling: 20,000 m (66,000 ft)
  • Rate of climb: 300 m/s (59,000 ft/min)
  • Wing loading: 406.7 kg/m2 (83.3 lb/sq ft)
  • Thrust/weight: 1.27

Armament

  • Guns: 1 x 30mm autocannon with up to 200 rounds
  • Hardpoints: 4 external hardpoints with a capacity of 8,000kg,with provisions to carry combinations of:
    • Rockets:
      • S-80 80mm unguided rockets
      • S-120 120mm unguided rockets
      • S-240 240mm unguided rockets
    • Missiles:
      • N06A Ruby short range AAM
      • N11A Spinel BVR AAM
      • N7S/L Crystal ALCM
      • N41S3 Chalcedony ASCM
      • N09S/L Topaz ASM
    • Bombs:
    • Other: external fuel tanks
  • Bombs: 3 internal weapons bays with a maximum capacity of 12,000 kilograms of ordnance.

See also

Aircraft of comparable role, configuration, and era