BASS - Aerospace Catalog (WIP|Do not Post)

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AEROSPACE PRODUCTS

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FIGHTERS

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• AR-3 "Fuego" Light Multirole Fighter - NSD 15 million
• AP-4 "Agila" Mediumweight Multirole Fourth Generation Fighter - NSD 49 million
• AP-7 "Draco" Heavy Multirole Fourth Generation Air superiority Fighter - NSD 55 million
• AP-9 "Ultra" Heavy Multirole Fifth Generation Air superiority Fighter - NSD 110 million

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BOMBERS

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LOGISTICAL AIRCRAFT

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HELICOPTERS

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MISCELLANEOUS

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AP-9 "Ultra" Heavy Multirole Fifth Generation Air superiority Fighter

The Ultra Fighter


Ultra AP9-C Carrier Variant

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General characteristics

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Crew: 1
Length: 20 m
Wingspan: 14 m
Inherent Weight: 19,750 kg
Maximum Fuel Weight: 35,656.25 kg

Performance specifications
Powerplant: 2 × Pratt & Whitney F100-PW-229 afterburning
turbofans equipped with Pratt & Whitney P/YBBN three-dimensional
thrust vectoring nozzles, 79 kN thrust dry, 129.7 kN with afterburner each
Maximum speed: Mach 2.42
Range: 2,100 km
Service ceiling: 18,600 m
Rate of climb: 318 m/s
Guns: 1 × 27mm Mauser BK-27 revolver autocannon in right
wing root, 130 rounds
Hardpoints: 3 × internal weapons bay, 1 on the bottom of the
fuselage and 2 on the sides of the fuselage, as well as 4 × underwing pylon stations

The AP9 "Ultra" is an advanced stealth, single-seat, twin-engine supermaneuverable multirole air superiority fighter developed by Ayala Aerospace Corporation and Dangan Corporation, together with Korea Aerospace Industries and Saab Group. First flew in early 204X and commissioned in late 204X, it was designed as a sophisticated lightweight fighter aircraft that is equipped with highly-sophisticated avionics and radar, powerful thrust-vectoring engines and stealth technology in order to satisfy the Bayan Hukwid's requirement for a next-generation cost-effective stealth fighter with the intention of supplementing and (later on) replacing prior-generation fighter aircraft within their aircraft inventory.

Featuring a large fuselage body and incorporating canted vertical stabilizers, all-moving horizontal tails, clipped delta wings and a retractable tricycle landing gear, the Ultra's airframe uses high-strength light alloy and carbon materials to withstand stress and heat of sustained supersonic flight. Radar absorbing materials in the form of durable fiber-mats along with the low-observable characteristics of the airframe shape significantly reduces the aircraft's radar cross-section (RCS). The Ultra has adjustable leading edge vortex controllers (LEVCONs) designed to control vortices generated by the leading edge root extensions, and can provide trim and improve high angle of attack behavior, including a quick stall recovery if the thrust vectoring system fails. To manage heat buildup from supersonic flight, the leading edges are equipped with active cooling. On the rear-left of the canopy, which uses a coating to deflect radar waves, is an in-flight refuelling probe.

The aircraft is equipped with various sophisticated avionics, the information management system being central to the avionic suite as it enhances man-machine interaction. The Ultra incorporates the Type 350 Integrated Helmet Display Sighting System into its system. The Type 350 is a helmet-mounted display system developed by the Scientific Military Research Bureau. First tested in late 1989 and introduced in early 1992, it is an upgraded derivative of the Type 340 IHDSS and is designed to be fitted on a flight helmet and allow pilots to obtain situation awareness and cue weapons systems to the direction their head is pointing, the Type 350 was created to be closely integrated with a combat aircraft's weapon system and operate in all-weather day/night flight environments. The system employs a quick digital processing package while retaining the same type of electromagnetic position sensing as the Type 340. Although the cathode ray tube package is very capable, it is limited to monochrome presentation of calligraphic symbology.

The Type 350 incorporates the various sensors of the aircraft and hence allows support for raster scanned imagery to display forward looking infrared (FLIR)/infra-red search and track (IRST) pictures for night operations and provides collimated symbology and imagery to the pilot. Part of the Ultra's avionics is that in addition to the integration of the aircraft's extensive sensor suite, data sharing from friendly external means allowing the pilot to view targets that could not be otherwise spotted using the aircraft's own sensors at the exclusion of everything else. It allows the pilot to view detected battlefield elements in the helmet that are beyond its own horizon and in blind sides of the aircraft where the Ultra's own body obscure's the pilot's view and it is by this means that the helmet display is able to give the pilot a comprehensive picture of the battlefield situation. An important part of the aircraft's fire-control system is the AN/APG-79 active electronically scanned array radar. Integrated position sensing ensures that symbols representing outside-world entities move in line with the pilot's head movements. The Ultra's electronics systems are hardened and 4 redundant systems have been composed to make the Ultra stand on the three remaining backup electronics systems in the face of systems failure therefore allowing a significant window for error even for the most testing of situations yet maintaining peak functionality. Apart from situational awareness and defense, the Ultra's AN/APG-79 AESA enables it to perform well as an EW platform tracking targets with low probability of intercept via a complicated pattern of frequency and amplitude modulations across a wide bandwidth.

The Ultra has three internal weapons bay, with one large bay located on the bottom of the fuselage and two smaller bays on the sides of the fuselage. The bottom bay is capable of carrying up to either four beyond-visual-range air-to-air missiles or two air-to-surface missiles. As for the side bays, each are capable of carrying a single short-range air-to-air missiles. During weapon launches, the bay doors would open for less than a second and the hydraulic arms push the weapons clear of the aircraft. An internally mounted Mauser BK-27 27mm autocannon is placed in the right wing root with a retractable door covering the muzzle, while each wing has two underwing pylon stations, although the use of external stores reduces the stealth and kinematic performance of the aircraft.

Variants

AP-9-A - The standard CTOL variant of the Ultra. Meant to replace the Sparrowhawk fighter fleet.

AP-9-C - The carrier variant of the Ultra. It features a fold-able wing with a larger wing area allowing for increased fuel capacity and hence longer operational range, a strengthened under carriage, stronger landing gear and tail hooks for carrier arrested landings. It also possesses software adjusted inward swept canards allowing for shorter takeoff distance and achieving high angle of attack for taking off and landing even on a low tech ski jump carrier. The canards vulnerable sharp facets are fitted with RAM to keep the integrity of the Ultra's stealth thereby maintaining the RCS less than that of a pinball. The Ultra C also has a much more cropped wing shape deviating from the original delta design. Instead, it adopts a lower wing aspect ratio in order to be more compact than its non carrier counterparts.

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AP-4 "Agila" Mediumweight Multirole Fourth Generation Fighter

The Agila Fighter

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General characteristics

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Length: 22 m
Wingspan: 18 m
Inherent Weight: 10,000 kg
Maximum Take-Off Weight: 22,000 kg

Performance specifications
Crew: 1
Powerplant: 2 × Pratt & Whitney F100-PW-220 afterburning turbofans,
64.9 kN thrust dry, 105.7 kN with afterburner each
Maximum speed: Mach 2.31
Range: 2,500 km
Service ceiling: 18,400 m
Rate of climb: 286 m/s
Guns: 1 × 27mm Mauser BK-27 revolver autocannon on the
right side of the fuselage, 120 rounds
Hardpoints: 6 × underwing stations and 3 × under fuselage

The AP4 "Punong Agila" is a twin-engine, single-seat, canard multirole fighter aircraft developed by Ayala Aerospace Corporation and Dangan Corporation, together with Korea Aerospace Industries and Saab Group. First flew in YEAR and commissioned in YEAR, it was designed as a medium-weight combat aircraft for the Bayan Hukwid (airforce) of the Philippines.

Featuring a conventional shoulder-mounted swept wing, rectangular side intakes, and a conventional tri-plane empennage arrangement with all-moving horizontal "stabilator" tailplanes, the Punong Agila is an aerodynamically unstable aircraft that uses digital fly-by-wire flight controls to artificially enforce and maintain stability. Two triangular shaped retractable surfaces are each mounted on the side of the fuselage, and can be automatically extended by the flight control system at high Mach numbers. They are used for generating additional lift (force) ahead of the aircraft's center of gravity, thus helping to compensate for mach tuck at supersonic speeds. Automatically deployed at above Mach 1.4, they allow the Punong Agila to pull 7.5 g at Mach 2 and could be manually extended as well. An aerial refuelling probe placed on the rear-right of the canopy enables further range extension.

The Punong Agila is equipped with the Israeli EL/M-2032 pulse-Doppler multimode planar array fire-control radar and features an infrared search and track (IRST) system in a retractable undernose fairing, as well as an electronic warfare support measures package.

Variants

AP4-A - The standard CTOL variant of the Agila.

AP4-B - The carrier variant of the Agila. It possesses foldable wingtips, strengthened landing gear, undercarriage and rare hooks as well as larger vertical stabilizers and wing area.

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AP-7 "Draco" Heavy Multirole Fourth Generation Air superiority Fighter

The Draco Fighter

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General characteristics

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Length: 22.6 m
Wingspan: 15.16 m
Inherent Weight: 16,375 kg
Maximum Take-Off Weight: 30,600 kg

Performance specifications
Powerplant: 2 × Yongsheng Type 29 afterburning turbofans,
78.4 kN thrust dry, 125.1 kN with afterburner each
Maximum speed: Mach 2.38
Range: 3,350 km
Service ceiling: 19,200 m
Rate of climb: 304 m/s
Guns: 1 × 27mm Mauser BK-27 revolver autocannon on the
left side of the fuselage, 150 rounds
Hardpoints: 10 in total - 8 × underwing stations and 2 × under fuselage

The AP7 "Draco" is a twin-engine, single-seat, multirole air superiority fighter aircraft developed by Ayala Aerospace Corporation and Dangan Corporation, together with Yongsheng Heavy Machinery Industries. First flew in early 204X and commissioned in late 204X, the aircraft features heavy ordnance, sophisticated avionics and long range in order to satisfy the Bayan Hukwid's requirement for a cost-effective heavy fighter aircraft.

Created with Zhouranese assistance, the Draco uses a highly-modified combination of the airframes of both the Jian-19-0-1 and Jian-20-1-0. A large twin-finned aircraft, the Draco is designed with trapezoidal wings and conventional horizontal tailplanes and is fitted with a fly-by-wire control system. An aerial refuelling probe enables further range extension.

The Draco is equipped with the Blue Sword (Putonghua: 蓝剑), a powerful, integrated, multi-mode dual frequency band, passive electronically scanned array radar from Zhouran. With a search range of 380 km, the radar can track 15 air targets and engage 4 simultaneously. The aircraft features an infrared search and track (IRST) system in the nose just forward of the cockpit, as well as an electronic warfare support measures package.

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AR-3 "Fuego" Light Multirole Fighter

The Fuego Fighter

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General characteristics

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Length: 14.57 m
Wingspan: 8.78 m
Inherent Weight: 7,031 kg
Maximum Take-Off Weight: 19,277 kg

Performance specifications
Powerplant: 1 × Pratt & Whitney F100-PW-220 afterburning turbofan,
64.9 kN thrust dry, 105.7 kN with afterburner
Maximum speed: Mach 1.6
Range: 2,100 km
Service ceiling: 18,300 m
Rate of climb: 225 m/s
Guns: 1 × 27mm Mauser BK-27 revolver autocannon in left
wing root, 130 rounds
Hardpoints: 6 × underwing stations and 1 × under fuselage

The AR3 "Fuego" is a single-engine, canard delta wing, multirole fighter aircraft developed by Ayala Aerospace Corporation and Dangan Corporation, together with Yongsheng Heavy Machinery Industries, Korea Aerospace Industries and Saab Group. First flew in 204X and commissioned in 204X, it was designed as a lightweight cost-effective fighter jet for the Bayan Hukwid (airforce) of the Philippines.

Combining a delta wing design with active close-coupled canard to maximize maneuverability, the Fuego is an aerodynamically unstable aircraft that uses digital fly-by-wire flight controls to artificially enforce and maintain stability. The forward fuselage of the aircraft is shaped in a manner that results in it naturally directing air into the engine intake and to avoid inlet blanking while flown at a sideslip condition. The engine air intake takes the form of a plain chin type scoop with a splitter plate. The wing is unusual in having a shallow sweep on the trailing edge, giving a fleche planform; the straight leading edge is swept at 54 degrees, with maneuver flaps on the outboard sections. Two piece flaperons occupies most of the trailing edge, which is blended into the fuselage with long fillets. The canards, located slightly astern of and below the pilot, cause minimal obstruction in vision and allow for pitch control in a single-piece, all-moving arrangement. A sharply swept vertical tail is mounted on a spine on top of the rear fuselage, and is supplemented by two steeply canted ventral strakes, mounted on the ends of the wing root fillets.

Designed to be cost-effective, agile and highly-maneuverable, the aircraft features electronic countermeasures and is equipped with the Israeli EL/M-2032 pulse-Doppler multimode planar array fire-control radar.