Aetherdyne Ae-16 Fuyuhana (Pacifica)

Ae-16 Fuyuhana
Role	Carrier-based strike fighter
National origin	Pelinai
Manufacturer	Aetherdyne IDB
First flight	November 18, 2004 (2004-11-18)
Introduction	March 7, 2009 (2009-03-07)
Status	In service
Primary user	Royal Pelinese Navy
Produced	August 9, 2003 – present (2003-08-09 – present)
Number built	Ae-16A/B/V/S/U: approx. 800+ (as of 2023)

The Aetherdyne Ae-16 Fuyuhana is a Pelinese carrier-cabale, twin-engine, all-weather strike fighter aircraft developed and manufactured by Pelinese aerospace bureau Aetherdyne. The Fuyuhana was developed to provide fleet defense and sea attack capabilities for aircraft carriers of the Royal Pelinese Navy, and is the standard tactical fighter aircraft of the Royal Pelinese Navy Air Service. Low-rate production of the type is ongoing as new airframes cycle in upgraded technology or replace planes lost to accidents, and over 800 airframes of all variants have been produced as of 2023.

The Fuyuhana was the first fixed-wing naval aircraft to be designed in Pelinai and the first to be operated by the Royal Pelinese Navy, with it taking its first flight in 2004 and receiving full adoption in 2009 alongside the newly commissioned KPF Pelograd. Various upgrade packages targeting electronics systems and other areas have allowed the Fuyuhana to maintain technological parity and resolve technical problems present in initial production models, and the type is expected to remain in active RPNAS service well into the 2040s.

Development

Background

The Royal Pelinese Navy first began identifying an outstanding procurement need for a series of fixed-wing naval aircraft in 1997, when it first implemented plans to steer its ongoing modernization initiatives towards the attainment of an carrier-based naval structure. Chief among these was what would later be referred to as the At-Sea Tactical Aircraft (ASTA), which was imagined as a medium-weight fighter that would primarily serve to provide air cover for Pelinese naval vessels while outside the range of land-based fighter support. As the primary aircraft necessitated by a carrier design that was then quickly gravitating towards a STOBAR configuration, the ASTA role was deemed to be the most likely candidate for navy adoption and was allocated the largest share of technical expertise.

Initial proposals for ASTA included searching for a suitable foreign-designed aircraft, as well designing a navalized variant for the currently serving Ae-12 Bara; a foreign aircraft purchase was quickly ruled out, however, and initial design studies concluded that the Bara could not be efficiently adapted to achieve the minimum stall speed and other performance standards necessary for the safe conduct of carrier takeoff and landing operations. Thus, after budgetary and technical considerations, the Pelinese Ministry of Defense opted to fund the development program for a new aircraft type to be operated by the Royal Pelinese Navy.

Variants

Production models

• Ae-16A: Initial production variant; the Ae-16A incorporated a PESA radar and conventional HUD. It suffered from many small technical and structural issues over its eight-year lifespan, contributing to a low ratio of flight hours to maintenance hours; all airframes of the A variant received a major overhaul in 2010 to correct a severe structural flaw in the design of the landing gear, and the type was fully withdrawn from service by 2017.
• Ae-16B:
• Ae-16V:
• Ae-16S:
• Ae-16U:

Specifications (Ae-16V)

General characteristics

• Crew: 1 (pilot)
• Length: 16.1 m (52 ft 10 in)
• Wingspan: 10.9 m (35 ft 9 in)
• Height: 4.3 m (14 ft 1 in)
• Wing area: 40.7 m² (438 sq ft)
• Empty weight: 15,000 kg (33,069 lb)
• Gross weight: 24,000 kg (52,911 lb)
• Max takeoff weight: 32,000 kg (70,548 lb)
• Fuel capacity: roughly 9,000kg internally
• Powerplant: 2 × Yuzimashi AF-13 afterburning low-bypass turbofan engines, 67 kN (15,000 lbf) thrust each dry, 109 kN (25,000 lbf) with afterburner

Performance

• Maximum speed: 2,450 km/h (1,520 mph, 1,320 kn)
• Maximum speed: Mach 2.0
• Cruise speed: 1,400 km/h (870 mph, 760 kn)
• Range: 2,400 km (1,500 mi, 1,300 nmi)
• Combat range: 1,200 km (750 mi, 650 nmi)
• Service ceiling: 17,000 m (56,000 ft)
• Rate of climb: 290 m/s (57,000 ft/min)
• Wing loading: 516.0 kg/m² (105.7 lb/sq ft)
• Thrust/weight: 1.06

Armament

• Guns: 1 x 30mm autocannon, 160 rounds
• Hardpoints: 4 x external hardpoints, 3 x internal weapons bays 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:
    • BVN-100, BVN-250, BVN-500, BVN-750, BVN-1000 gravity bombs
    • Laser, satellite guided bombs
    • Cluster bombs
    • N91B Prasiolite anti-runway bombs
    • N12B Rose Quartz guided anti-fortification bombs
  • Other: external fuel tanks
• Bombs: 3 internal weapons bays with a maximum capacity of 2,000 kilograms of ordnance.

Avionics

• Sensors:
• Pelektronik ATP-3A AESA radar
• Electro-optical targeting system
• IRST sensor array
• Defensive systems:
• ECM system
• Combination IR/UV missile approach detector
• Radar warning receiver
• Towed radar decoys
• CNI systems:
• High-speed datalink transceiver
• Multifunction radio
• TACAN
• Pilot support systems:
• Helmet-mounted pilot night vision system
• Type 014 helmet-mounted display/sight system