Mgellis
Posts: 2054
Joined: 8/18/2007 Status: offline
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[ADDED DB v440 (...except Canadair Sabre)] Additional aircraft for Honduras... Lockheed C-130A/D Hercules Operational dates: 1987-present F-5E/F Freedom Fighter Operational dates: 1988-present Canadair Sabre (they got 10 from Yugoslavia, of all places) Operational dates: 1976-1987 (Information from Wikipedia) General characteristics Crew: one, pilot Length: 37 ft 6 in (11.43 m) Wingspan: 37 ft 1½ in (11.32 m) Height: 14 ft 9 in (4.49 m) Empty weight: 10,618 lb (4,816 kg) Max. takeoff weight: 17,560 lb (7,965 kg) Powerplant: 1 × Avro Canada Orenda 14 turbojet, 7,275 lbf (32.36 kN) Performance Maximum speed: 710 mph (1142 km/h) Range: 1,270 mi (2044 km) Service ceiling: 54,000 ft (16,460 m) Rate of climb: 11,800 ft/min (59.9 m/s) Armament Guns: 6 0.50 in (12.7 mm) M3 Browning machine guns (1,602 rounds in total) Rockets: variety of rocket launchers; e.g: 2 Matra rocket pods with 18 SNEB 68 mm rockets per pod Missiles: 2 AIM-9 Sidewinders Bombs: 5,300 lb (2,400 kg) of payload on four external hardpoints, bombs are usually mounted on outer two pylons as the inner pairs are wet-plumbed pylons for 2 200 US gallons (760 L) drop tanks to give the Sabre a useful range. A wide variety of bombs can be carried (max standard loadout being 2 1,000 lb bombs plus 2 drop tanks), napalm bomb canisters and can include a tactical nuclear weapon. Bell 412SP Operational dates: 1986-present General characteristics Crew: 1-2 pilots Capacity: up to 13 passengers, maximum external load of almost 6,614 lb (3,000 kg)[41] Length: 56 ft 1 in (17.1 m) Rotor diameter: 46 ft (14.0 m) Height: 15 ft (4.6 m) Disc area: 1,662 ft² (154.4 m²) Empty weight: 6,789 lb (3,079 kg) Max. takeoff weight: 11,900 lb (5,397 kg) Powerplant: 2 × Pratt & Whitney Canada PT6T-3BE Twin-Pac turboshafts, 900 shp (671 kW) each Fuselage length: 43 ft (13.1 m) Performance Maximum speed: 140 knots (161 mph, 259 km/h) Cruise speed: 122 knots (140 mph, 226 km/h) Range: 609 mi (up to 980km) Service ceiling: 20,000 ft (6,096 m) Rate of climb: 1,350 ft/min (6.86 m/s) Power/mass: 0.2663 hp/lb (437 W/kg) (Wikipedia says the 412SP is a "Special Performance version with P&WC PT6T-3BF engines") Super Mystère B.2 Operational dates: 1976-1987 General characteristics Crew: 1 Length: 14.13 m (46 ft 4 in) Wingspan: 10.51 m (34 ft 6 in) Height: 4.6 m (15 ft 1 in) Wing area: 32.0 m² (344 ft²) Empty weight: 6,390 kg (14,090 lb) Loaded weight: 9,000 kg (20,000 lb) Max. takeoff weight: 10,000 kg (22,000 lb) Fuel capacity: 2,000 kg (4,400 lb) Powerplant: 1 × SNECMA Atar 101G-2 turbojet Dry thrust: 33.3 kN (7,490 lbf) Thrust with afterburner: 44.1 kN (9,920 lbf) Performance Maximum speed: Mach 1.12 (1,195 km/h, 743 mph) at 11,000 m (36,000 ft) Combat range: 870 km (470 NM, 540 mi) Ferry range: 1,175 km (634 NM, 730 mi) Service ceiling: 17,000 m (56,000 ft) Rate of climb: 89 m/s (18,000 ft/min) Wing loading: 281 kg/m² (57.6 lb/ft²) Thrust/weight: 0.50 Armament Guns: 2× 30 mm (1.18 in) DEFA 552 cannons with 150 rounds per gun Rockets: 2× Matra rocket pods with 18× SNEB 68 mm rockets each Missiles: 2× Rafael Shafrir AAMs; 2× AS-30L Bombs: 2,680 kg (5,000 lb) of payload on four external hardpoints, including a variety of bombs, reconnaissance pods or Drop tanks Thanks for considering these! (Some additional information from http://www.scramble.nl/orbats/honduras/overview)
< Message edited by emsoy -- 8/22/2015 11:08:07 PM >
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