Na-17 Marahu (Pacifica)
| Na-17 Marahu | |
|---|---|
| Role | Strategic bomber |
| National origin |  Pelinai
|
| Manufacturer | Nanohi IDB |
| First flight | June 23, 1998 |
| Introduction | February 20, 2003 |
| Primary user |  Royal Pelinese Air Force
|
| Number built | 112 |
The Nanohi Na-17 Marahu is a variable-sweep wing, supersonic heavy bomber operated by the Royal Pelinese Air Force. 108 airframes of 3 variants are in active or reserve service under the RPAF Strike Forces Command.
Intended combat roles for the Na-17 Marahu include strategic bombing of hardened military facilities and maritime strike bombing. The Marahu’s long range, high speed, and relatively low observability are intended to increase its survivability and chances of success in deep strike missions against high-value, heavily defended military targets such as capital ships, ICBM launch silos, command bunkers, and airfields. Delivery of nuclear weapons is also possible, and the Na-17 is used as part of the PAF’s nuclear deterrent capability.
Development
The Na-17 Marahu’s development program began in 1993 as a proposed candidate for the “Long-Range Strategic Strike Bomber” requirement of the RPAF. Initial program requirements set forth by the Procurement & Materiel Command included a minimum combat-load range of 8,000 kilometers, a cruise speed above mach 1.3, low-level penetration bombing capability, and a maximum ordnance load of 48,000 kilograms in internal weapons bays. High payload, range, and cruise speed requirements together required the adoption of a large heavy bomber design mounting multiple low-bypass afterburning turbofan engines; designers also incorporated a variable-sweep wing to match conflicting performance requirements at different altitudes and speeds. Later merging of the LRSSB project with a similar development program for a maritime strike bomber also led to the addition of 6 external hardpoints to the prototype design in order to carry large anti-ship cruise missiles. The first prototype model, the Na-17X1, was capable of carrying 66,000 kilograms of ordnance between its internal weapons bays and its external hardpoints as well as maintaining a cruise speed of 1,800km/h at altitude. Testing of 4 prototypes revealed a fault in the linkage mechanism between the wings and fuselage, which resulted in the loss of 1 prototype in a testing accident and a reduction in the production model’s payload capacity of 2,000 kilograms due to added structural reinforcements.
Design
Airframe
Notable design features of the production model Na-17 Marahu include a blended wing-body airframe combined with a variable sweep wing, a conventional tailplane and rudder, and small canards on the forward nose. Four Yunimashi AF-19 turbofans developed specifically for the Na-17 provide the aircraft’s thrust and are mounted on the underside of the fuselage in pairs. The sweep angle on the wings can be varied from 15° to 65°. The Na-17 has an unusually small radar cross-section for its size due to numerous stealth features, including serrated panels, engine compressor blade shielding, and radar-absorbing outer panels, and is roughly comparable in radar visibility to an air superiority fighter.
Armament
The external hardpoints have a maximum payload capacity of 4,000 kilograms each, rendering each one capable of carrying 1 heavy anti-ship cruise missile, 2 land attack cruise missiles, 6 air-to-surface missiles, 2 2,000kg bombs, or other ordnance packages. The internal weapons bays have a combined payload capacity of 40,000 kilograms and are used to carry guided and unguided bombs. The use of all types of missiles and precision-guided munitions is supported in the Na-17M variant.
Avionics
Notable electronics and avionics systems mounted on the Na-17 include an AESA radar, an ECM suite, and secondary mounting points for additional bomb targeting designators.
Upgrades
Initial upgrades and retrofits to the Na-17P Marahu occurred in 2006 and included the replacement of the previous R-09T PESA targeting radar with the newly designed R-10T AESA ground attack radar, the addition of integrated target designation equipment and interface support for the use of precision-guided munitions, and an overhaul of the ECM package. The Na-17V and Na-17M variants add various modernized electronics and fault corrections to the original aircraft.
Specifications (Na-17M)
General characteristics
- Crew: 4: aircraft commander, pilot, two aircraft systems officers
- Length: 45 m (147 ft 8 in)
- Wingspan: 43 m (141 ft 1 in)
- Swept wingspan: 24.5 m (80 ft 5 in) swept
- Height: 10 m (32 ft 10 in)
- Wing area: 190 m2 (2,000 sq ft)
- Empty weight: 90,000 kg (198,416 lb)
- Gross weight: 150,000 kg (330,693 lb)
- Max takeoff weight: 214,000 kg (471,789 lb)
- Fuel capacity: roughly 49,000 liters
- Powerplant: 4 × Yunimashi AF-19 afterburning low-bypass turbofan engines, 140 kN (31,000 lbf) thrust each dry, 205 kN (46,000 lbf) with afterburner
Performance
- Maximum speed: 2,500 km/h (1,600 mph, 1,300 kn)
- Maximum speed: Mach 2.0
- Cruise speed: 1,800 km/h (1,100 mph, 970 kn)
- Range: 10,000 km (6,200 mi, 5,400 nmi)
- Combat range: 7,000 km (4,300 mi, 3,800 nmi)
- Service ceiling: 17,000 m (56,000 ft)
- Rate of climb: 45 m/s (8,900 ft/min)
- Wing loading: 816 kg/m2 (167 lb/sq ft)
- Thrust/weight: 0.38
Armament
- Guns: none
- Hardpoints: 6 external hardpoints with a capacity of 24,000kg,with provisions to carry combinations of:
- Missiles:
- 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
- Naval mines
- Landmines
- Bombs: 3 internal weapons bays with a maximum capacity of 40,000 kilograms of ordnance.
Distinctive features
Variable-geometry wing blended to fuselage; four Yunimashi AF-19 turbofans in under-fuselage pods; small canards
Variants & Operators
Prototype Na-17X1 first flown in 1998; RPAF took delivery of first serial production model Na-17P in 2003. 112 aircraft of all variants were produced, of which 108 are still in service or reserve under the RPAF.