|
Join the AAF Cartographer: Vlaskovic Historian: Artstotszka Guardian: Freechrist |
![]() Founded: January 20th, 2016 Motto:Where Dreams Become Story. We prefer a small closely-knit active community, than that of a large inactive loose-knit community |
The regional roleplays now can be found on the region's Regional Roleplay Dispatch that's pinned onto the WFE. |
Welcome to Audaxia. We hope you enjoy your visit. You're currently viewing our forum as a guest. This means you are limited to certain areas of the board and there are some features you can't use. If you join our community, you'll be able to access member-only sections, and use many member-only features such as customizing your profile, sending personal messages, and voting in polls. Registration is simple, fast, and completely free. Join our community! If you're already a member please log in to your account to access all of our features: |
The Kingdom of Gondor Armed Forces | |
---|---|
Topic Started: Apr 7 2016, 03:41 AM (322 Views) | |
Gondor | Apr 7 2016, 03:41 AM Post #1 |
![]()
![]() |
SU-35 Type: Air Superiority Fighter Specifications: Crew: 1 Length: 21.9 m (72.9 ft) Wingspan: 15.3 m (50.2 ft, with wingtip pods) Height: 5.90 m (19.4 ft) Wing area: 62.0 m² (667 ft²) Empty weight: 18,400 kg (40,570 lb) Loaded weight: 25,300 kg (56,660 lb) at 50% internal fuel Max. takeoff weight: 34,500 kg (76,060 lb) Powerplant: 2 × Saturn 117S (AL-41F1S) afterburning turbofan with 3D thrust vectoring nozzle Dry thrust: 8,800 kgf (86.3 kN, 19,400 lbf) each Thrust with afterburner: 14,500 kgf (142 kN, 31,900 lbf) each Fuel capacity: 11,500 kg (25,400 lb) internally Performance Maximum speed: At altitude: Mach 2.25 (2,390 km/h, 1,490 mph) At sea level: Mach 1.15 (1,400 km/h, 870 mph) Range: At altitude: 3,600 km (1,940 nmi) At sea level: 1,580 km (850 nmi) Ferry range: 4,500 km (2,430 nmi) with 2 external fuel tanks Service ceiling: 18,000 m (59,100 ft) Rate of climb: >280 m/s (>55,000 ft/min) Wing loading: 408 kg/m² (500.8 kg/m² with full internal fuel) (84.9 lb/ft² 50% fuel) Thrust/weight: 1.13 at 50% fuel (0.92 with full internal fuel) Maximum g-load: +9 g Armament Guns: 1× 30 mm GSh-301 internal cannon with 150 rounds Hardpoints: 12 hardpoints, consisting of 2 wingtip rails, and 10 wing and fuselage stations with a capacity of 8,000 kg (17,630 lb) of ordnance and provisions to carry combinations of: Rockets: S-25L laser-guided rocket S-25 unguided rocket B-8 unguided S-8 rocket pods B-13 unguided S-13 rocket pods Missiles: Vympel R-73E/M, and R-74M Vympel R-27R/ER/T/ET Vympel R-77 – the proposed R-77M, R-77T, K-77M Vympel R-37M[160] Kh-29T/L Kh-31P/A Kh-59ME Bombs: KAB-500L laser-guided bomb KAB-1500L laser-guided bomb FAB-250 250-kilogram (550 lb) unguided bombs FAB-500 500-kilogram (1,100 lb) unguided bombs Other: buddy refueling pod Avionics Irbis-E passive phased array radar OLS-35 infra-red search and track system L265 Khibiny-M electronic warfare pod APG-81 AESA Radar ![]() MIG-35 Type: Multirole Fighter/Interdiction Crew: 1 or 2 Length: 17.3 m (56 ft 9 in) Wingspan: 12 m (39 ft 4 in) Height: 4.7 m (15 ft 5 in) Wing area: 38 m2 (409 ft2) Empty weight: 11,000 kg (24,250 lb) Loaded weight: 17,500 kg (38,600 lb) Max. takeoff weight: 29,700 kg (65,500 lb) Powerplant: 2 × Klimov RD-33MK afterburning turbofans Dry thrust: 5,400 kgf, 53.0 kN (11,900 lbf) each Thrust with afterburner: 9,000 kgf, 88.3 kN (19,840 lbf) each Performance Maximum speed: Mach 2.25 (2,400 km/h, 1,491 mph) at altitude;[34] 1,450 km/h (901 mph) at low-level Range: 2,000 km (1,240 mi) Combat radius: 1,000 km (620 mi) Ferry range: 3,100 km (1,930 mi) with 3 external fuel tanks Service ceiling: 17,500 m (57,400 ft) Rate of climb: 330 m/s (65,000 ft/min[36]) Thrust/weight: 1.03[37] Max. maneuvering load factor: 10.0 g[35] Armament Guns: 1× 30 mm GSh-30-1 cannon, 150 rounds Hardpoints: 9 total (8× under-wing, 1× centre-line) with a capacity of 7,000 kg[10] Rockets: S-8, S-13, S-24, S-25L, S-250 unguided and laser-guided rockets Missiles: Air-to-air: AA-10 Alamo: 4× R-27R, R-27T, R-27ER, R-27ET AA-8 Aphid: 4× R-60M AA-11 Archer: 8× R-73E, R-73M, R-74M AA-12 Adder: 8× R-77 Air-to-surface: AS-17 Krypton: 4× Kh-31A, Kh-31P AS-14 Kedge: 4× Kh-29T, Kh-29L Bombs: Guided: KAB-500L: 500 kg laser-guided bomb KAB-500T: 500 kg TV-guided bomb Unguided: FAB-250: 250 kg bomb FAB-500: 500 kg bomb ZAB-500 fuel-air explosive Bomb Avionics Phazotron Zhuk AE AESA radar (or other members of the Zhuk radar family) NII PP OLS-UEM Optical Location station ![]() Tu-160 Type: Supersonic Heavy Bomber Specifications: Crew: 4 (pilot, co-pilot, bombardier, defensive systems operator) Length: 54.10 m (177 ft 6 in) Wingspan: Spread (20° sweep): 55.70 m (189 ft 9 in) Swept (65° sweep): 35.60 m (116 ft 9¾ in) Height: 13.10 m (43 ft 0 in) Wing area: Spread: 400 m² (4,306 ft²) Swept: 360 square metres (3,900 sq ft)) Empty weight: 110,000 kg (242,505 lb; operating empty weight) Loaded weight: 267,600 kg (589,950 lb) Max. takeoff weight: 275,000 kg (606,260 lb) Powerplant: 4 × Samara NK-321 turbofans Dry thrust: 137.3 kN (30,865 lbf) each Thrust with afterburner: 245 kN (55,115 lbf) each Performance Maximum speed: Mach 2.05 (2,220 km/h, 1,200 knots, 1,380 mph) at 12,200 m (40,000 ft) Cruise speed: Mach 0.9 (960 km/h, 518 knots, 596 mph) Range: 12,300 km (7,643 mi) practical range without in-flight refuelling, Mach 0.77 and carrying 6 × Kh-55SM dropped at mid range and 5% fuel reserves[68] Combat radius: 7,300 km[69] (3,994 nmi, 4,536 mi,) 2,000 km (1,080 nmi, 1,240 mi) at Mach 1.5[29] Service ceiling: 15,006 m (49,235 ft) Rate of climb: 70 m/s (13,860 ft/min) Wing loading: 742 kg/m² with wings fully swept (152 lb/ft²) lift-to-drag: 18.5–19, while supersonic it is above 6.[70] Thrust/weight: 0.37 Armament Two internal bays for 40,000 kg (88,185 lb) of ordnance including Two internal rotary launchers each holding 6× Raduga Kh-55SM/101/102/555 cruise missiles (primary armament) or 12× AS-16 Kickback short-range nuclear missiles. ![]() MIG-31 Type: Interceptor Specifications: Crew: Two (pilot and weapons system officer) Length: 22.69 m (74 ft 5 in) Wingspan: 13.46 m (44 ft 2 in) Height: 6.15 m (20 ft 2 in) Wing area: 61.6 m2 (663 ft2) Empty weight: 21,820 kg (48,100 lb) Loaded weight: 41,000 kg (90,400 lb) Max. takeoff weight: 46,200 kg (101,900 lb) Powerplant: 2 × Soloviev D-30F6 afterburning turbofans Dry thrust: 93 kN (20,900 lbf) each Thrust with afterburner: 152 kN (34,172 lbf) each Performance Maximum speed: High altitude: Mach 2.83 (3,000 km/h, 1,860 mph)[6] Low altitude: Mach 1.2 (1,500 km/h, 930 mph) Cruise speed: Mach 2.35 (2,500 km/h; 1,550 mph) Combat radius: 1,450 km (900 mi) at Mach 0.8 and at altitude of 10,000 m (33,000 ft); 720 km (450 mi) at Mach 2.35 and altitude of 18,000 m (59,000 ft)[95] Combat range: 3,000 km[96] (1,860 mi) with 4xR-33E and 2 drop tanks; 5,400 km (3,360 mi) with 4xR-33E and 2 drop tanks with one in-flight refueling[96] Service ceiling: 20,600 m (67,600 ft) Rate of climb: 208 m/s (41,000 ft/min) Wing loading: 665 kg/m2 (136 lb/ft2) Thrust/weight: 0.85 Maximum g-load: 5 g Armament MiG-31BM 1× GSh-6-23 23 mm cannon with 260 rounds. Fuselage recesses for either:[2] 4× R-33 (AA-9 'Amos') 4x R-33S 4x R-37M (AA-13 'Arrow') 4 underwing pylons for either:[2] 2 or 4x R-40 (AA-6 'Acrid') MVR AAM 4× R-73 (AA-11 'Archer') WVR AAM 4× R-77-1 (AA-12 'Adder') BVR AAM ![]() SU-34 Type: Strike Fighter, Fighter/Bomber Specifications: Length: 23.34 m (72 ft 2 in) Wingspan: 14.7 m (48 ft 3 in) Height: 6.09 m (19 ft 5 in) Wing area: 62.04 m² (667.8 ft²) Empty weight: 22,500 kg (49,608 lb) Loaded weight: 39,000 kg (85,980 lb) Max. takeoff weight: 45,100 kg (99,425 lb) Powerplant: 2 × 13,500 kgf (132 kN, 29,762 lbf) afterburning thrust Lyulka AL-31FM1[99] turbofans Internal fuel: 12,100 kg (15,400 l) Performance Maximum speed: High altitude: Mach 1.8+ (≈2,000 km/h, 1,200 mph) Low altitude: Mach 1.2 (1,400 km/h, 870 mph) at sea level Cruise speed: unknown Range: 1,100 km (680 mi) at low level altitude Combat radius: 1,000+ km (about 680 mi) Ferry range: 4,000 km (2,490 mi) Service ceiling: 15,000 m (49,200 ft) Thrust/weight: 0.68 Maximum g-load: 9g[100] Armament Guns: 1× 30 mm GSh-30-1 (9A-4071K) cannon, 150–180 rounds[101] Hardpoints: 12× wing and fuselage stations with a capacity of 8,000–12,000 kg (17,600–26,500 lb)[102][55] and provisions to carry combinations of: Rockets: S-8, S-13, S-25 rocket pods Missiles: R-27 (AA-10) air-to-air missile R-73 (AA-11) air-to-air missile R-77 (AA-12) air-to-air missile Kh-29L/T (AS-14) air-to-ground missile Kh-38 new generation air-to-ground missile with a range of 40 km Kh-25MT/ML/MP (AS-10) air-to-ground missile or anti-radiation missile Kh-59M (AS-18) air-to-ground missile Kh-58 (AS-11) anti-radiation missile Kh-31 (AS-17) anti-radiation or anti-ship missile Kh-35 (AS-20) anti-ship missile P-800 Oniks missile (SS-N-26 Strobile) anti-ship missile (version for the Air Force). Version named "Alpha",[103] weight of 1500 kg with a range of up to 300 km and a speed in the range of numbers M = 2.2-3.0. Officially not in service.[103][104] Kh-65SE or Kh-SD cruise missile Bombs: KAB-500L, KAB-500KR, KAB-500S and KAB-1500L/KR guided bombs OFAB-250-270, OFAB-100-120, FAB-500T, BETAB-500SHP, P-50T, ODAB-500PM unguided bombs, RBK-500 and SPBE-D cluster bombs, tactical nuclear bombs Other: 3,000 litres PTB-3000 Suspended Fuel Tanks, EW and reconnaissance pods. Edited by Gondor, Apr 7 2016, 03:43 PM.
|
![]() ![]() |
![]() ![]() |
Gondor | Apr 7 2016, 03:30 PM Post #2 |
![]()
![]() |
Saab JAS 39 Gripen Type: Carrier-based Air Superiority Fighter Specifications: Crew: 1 (2 for JAS 39D) Payload: 5,300 kg (11,700 lb) Length: 14.1 m (46 ft 3 in); two-seater: 14.8 m (48 ft 5 in) Wingspan: 8.4 m (27 ft 7 in) Height: 4.5 m (14 ft 9 in) Wing area: 30.0 m² (323 ft²) Empty weight: 6,800 kg[330] (14,990 lb) Loaded weight: 8,500 kg (18,700 lb) Max. takeoff weight: 14,000 kg (31,000 lb) Powerplant: 1 × Volvo RM12 afterburning turbofan Dry thrust: 54 kN (12,100 lbf) Thrust with afterburner: 80.5 kN (18,100 lbf) Wheel track: 2.4 m (7 ft 10 in) Performance Maximum speed: Mach 2 (2,204 km/h (1,190 kn; 1,370 mph)) at high altitude Combat radius: 800 km (497 mi, 432 nmi) Ferry range: 3,200 km (1,983 mi) with drop tanks Service ceiling: 15,240 m (50,000 ft) Wing loading: 283 kg/m² (58 lb/ft²) Thrust/weight: 0.97 Maximum g-load: +9 g Armament Guns: 1× 27 mm Mauser BK-27 Revolver cannon with 120 rounds (single-seat models only) Hardpoints: 8 (three on each wing and two under fuselage) and provisions to carry combinations of: Rockets: 4× rocket pods, 13.5 cm rockets Missiles: 6× AIM-9 Sidewinder (Rb.74) or IRIS-T (Rb 98) or A-Darter 4× AIM-120 AMRAAM (Rb.99) or MICA 4× Meteor (under development) 4× AGM-65 Maverick (Rb.75) 2× KEPD.350 2× Rbs.15F anti-ship missile Bombs: 4× GBU-12 Paveway II laser-guided bomb 2× Bk.90 cluster bomb 8× Mark 82 bombs ![]() MI-26 Type: Transport and Utility Helicopter Specifications: Crew: Five: 2 pilots, 1 navigator, 1 flight engineer, 1 flight technician Capacity: 90 troops or 60 stretchers 20,000 kg cargo (44,090 lb) Length: 40.025 m (131 ft 3¾ in) (rotors turning) Rotor diameter: 32.00 m (105 ft 0 in) Height: 8.145 m (26 ft 8¾ in) Disc area: 804.25 m2 (8,656.8 ft²) Empty weight: 28,200 kg (62,170 lb) Loaded weight: 49,600 kg (109,350 lb) Max. takeoff weight: 56,000 kg (123,450 lb) Powerplant: 2 × Lotarev D-136 turboshafts, 8,500 kW (11,399 shp) each Main rotor RPM: 132 Performance Maximum speed: 295 km/h (159 kn, 183 mph) Cruise speed: 255 km/h (137 kn, 158 mph) Range: 1,920 km (1,036 nmi, 1,190 mi) (with auxiliary tanks) Service ceiling: 4,600 m (15,100 ft) ![]() C-5 Galaxy Type: Strategic Airlifter Specifications: Crew: 7 typical (aircraft commander, pilot, two flight engineers, three loadmasters) 4 minimum (pilot, copilot, two flight engineers) Payload: 270,000 lb (122,470 kg) Length: 247 ft 1 in (75.31 m) Wingspan: 222 ft 9 in (67.89 m) Height: 65 ft 1 in (19.84 m) Wing area: 6,200 ft2 (576 m2) Empty weight: 380,000 lb (172,370 kg) Loaded weight: 769,000 lb (348,800 kg) Max. takeoff weight: 840,000 lb (381,000 kg) Powerplant: 4 × General Electric TF39-GE-1C high-bypass turbofan, 43,000 lbf (190 kN) each Performance Maximum speed: Mach 0.79 (503 kn, 579 mph, 932 km/h) Cruise speed: Mach 0.77 (496 kn, 571 mph, 919 km/h) Range: 2,400 nmi (2,760 mi, 4,440 km) with a 263,200 lb (119,400 kg) payload Service ceiling: 35,700 ft (10,600 m) at 615,000 lb (279,000 kg) gross weight Rate of climb: 1,800 ft/min (9.14 m/s) Wing loading: 120 lb/ft2 (610 kg/m2) Thrust/weight: 0.22 Takeoff roll: 8,400 ft (2,600 m) Landing roll: 3,600 ft (1,100 m) Fuel capacity: 51,150 US gal (193,600 L) ![]() C-17 Globemaster III Type: Strategic and Tactical Airlifter Specifications: Crew: 3: 2 pilots, 1 loadmaster (five additional personnel required for aeromedical evacuation) Capacity: 102 paratroopers or 134 troops with palletized and sidewall seats or 54 troops with sidewall seats (allows 13 cargo pallets) only or 36 litter and 54 ambulatory patients and medical attendants or Cargo, such as an M1 Abrams tank, three Strykers, or six M1117 Armored Security Vehicles Payload: 170,900 lb (77,519 kg) of cargo distributed at max over 18 463L master pallets or a mix of palletized cargo and vehicles Length: 174 ft (53 m) Wingspan: 169.8 ft (51.75 m) Height: 55.1 ft (16.8 m) Wing area: 3,800 ft² (353 m²) Empty weight: 282,500 lb (128,100 kg) Max. takeoff weight: 585,000 lb (265,350 kg) Powerplant: 4 × Pratt & Whitney F117-PW-100 turbofans, 40,440 lbf (180 kN) each Fuel capacity: 35,546 U.S. gal (134,556 L) Performance Cruise speed: Mach 0.74 (450 knots, 515 mph, 830 km/h) Range: 2,420 nmi[192] (2,785 mi, 4,482 km) ; 5,610 nmi (10,390 km) with paratroopers Service ceiling: 45,000 ft (13,716 m) Max. wing loading: 150 lb/ft² (750 kg/m²) Minimum thrust/weight: 0.277 Takeoff run at MTOW: 7,600 ft (2,316 m)[192] Landing distance: 3,500 ft (1,060 m) ![]() A-10 Warthog Type: Ground Attack Aircraft Specifications: Crew: 1 Length: 53 ft 4 in (16.26 m) Wingspan: 57 ft 6 in (17.53 m) Height: 14 ft 8 in (4.47 m) Wing area: 506 ft² (47.0 m²) Airfoil: NACA 6716 root, NACA 6713 tip Empty weight: 24,959 lb (11,321 kg) Loaded weight: 30,384 lb (13,782 kg) CAS mission: 47,094 lb (21,361 kg) Anti-armor mission: 42,071 lb (19,083 kg) Max. takeoff weight: 50,000 lb (23,000 kg) Powerplant: 2 × General Electric TF34-GE-100A turbofans, 9,065 lbf (40.32 kN) each Internal fuel capacity: 11,000 lb (4,990 kg) Performance Never exceed speed: 450 knots (518 mph,[162] 833 km/h) at 5,000 ft (1,500 m) with 18 Mk 82 bombs[163] Maximum speed: 381 knots (439 mph, 706 km/h) at sea level, clean[162] Cruise speed: 300 knots (340 mph, 560 km/h) Stall speed: 120 knots (138 mph, 220 km/h) [164] Combat radius: CAS mission: 250 nmi (288 mi, 460 km) at 1.88 hour loiter at 5,000 ft (1,500 m), 10 min combat Anti-armor mission: 252 nmi (290 mi, 467 km), 40 nmi (45 mi, 75 km)) sea-level penetration and exit, 30 min combat Ferry range: 2,240 nmi (2,580 mi, 4,150 km) with 50 knot (55 mph, 90 km/h) headwinds, 20 minutes reserve Service ceiling: 45,000 ft (13,700 m) Rate of climb: 6,000 ft/min (30 m/s) Wing loading: 99 lb/ft² (482 kg/m²) Thrust/weight: 0.36 Armament Guns: 1× 30 mm (1.18 in) GAU-8/A Avenger Gatling cannon with 1,174 rounds (Capacity 1,350) Hardpoints: 11 (8× under-wing and 3× under-fuselage pylon stations) with a capacity of 16,000 lb (7,260 kg) and provisions to carry combinations of: Rockets: 4× LAU-61/LAU-68 rocket pods (each with 19× / 7× Hydra 70 mm rockets, respectively) 4× LAU-5003 rocket pods (each with 19× CRV7 70 mm rockets) 6× LAU-10 rocket pods (each with 4× 127 mm (5.0 in) Zuni rockets) Missiles: 2× AIM-9 Sidewinders air-to-air missiles for self-defense 6× AGM-65 Maverick air-to-surface missiles Bombs: Mark 80 series of unguided iron bombs or Mk 77 incendiary bombs or BLU-1, BLU-27/B Rockeye II, Mk20, BL-755[165] and CBU-52/58/71/87/89/97 cluster bombs or Paveway series of Laser-guided bombs or Joint Direct Attack Munition (A-10C)[166] or Wind Corrected Munitions Dispenser (A-10C) Other: SUU-42A/A Flares/Infrared decoys and chaff dispenser pod or AN/ALQ-131 or AN/ALQ-184 ECM pods or Lockheed Martin Sniper XR or LITENING targeting pods (A-10C) or 2× 600 US gallon Sargent Fletcher drop tanks for increased range/loitering time. Avionics AN/AAS-35(V) Pave Penny laser tracker pod[167] (mounted beneath right side of cockpit) for use with Paveway LGBs (Currently the Pave Penny is no longer in use) Head-up display (HUD) for improved technical flying and air-to-ground support.[168] ![]() Edited by Gondor, Apr 7 2016, 03:48 PM.
|
![]() ![]() |
![]() ![]() |
Gondor | Apr 7 2016, 03:39 PM Post #3 |
![]()
![]() |
AH-64 Apache Type: Attack Helicopter Specifications: Crew: 2 (pilot, and co-pilot/gunner) Length: 58.17 ft (17.73 m) (with both rotors turning) Rotor diameter: 48 ft 0 in (14.63 m) Height: 12.7 ft (3.87 m) Disc area: 1,809.5 ft² (168.11 m²) Empty weight: 11,387 lb (5,165 kg) Loaded weight: 17,650 lb (8,000 kg) Max. takeoff weight: 23,000 lb (10,433 kg) Powerplant: 2 × General Electric T700-GE-701 turboshafts, 1,690 shp (1,260 kW) [upgraded to T700-GE-701C (for AH-64A/D from 1990), 1,890 shp (1,409 kW)] each Fuselage length: 49 ft 5 in (15.06 m) Rotor systems: 4 blade main rotor, 4 blade tail rotor in non-orthogonal alignment Performance Never exceed speed: 197 knots (227 mph, 365 km/h) Maximum speed: 158 knots (182 mph, 293 km/h) Cruise speed: 143 knots (165 mph, 265 km/h) Range: 257 nmi (295 mi, 476 km) with Longbow radar mast Combat radius: 260 nmi (300 mi, 480 km) Ferry range: 1,024 nmi (1,180 mi, 1,900 km) Service ceiling: 21,000 ft (6,400 m) minimum loaded Rate of climb: 2,500 ft/min (12.7 m/s) Disc loading: 9.80 lb/ft² (47.9 kg/m²) Power/mass: 0.18 hp/lb (0.31 kW/kg) Armament Guns: 1× 30 mm (1.18 in) M230 Chain Gun with 1,200 rounds as part of the Area Weapon Subsystem Hardpoints: Four pylon stations on the stub wings. Longbows also have a station on each wingtip for an AIM-92 Stinger twin missile pack.[70] Rockets: Hydra 70 70 mm, CRV7 70 mm, and APKWS 70 mm[69] air-to-ground rockets Missiles: Typically AGM-114 Hellfire variants; AIM-92 Stinger may also be carried. Avionics Lockheed Martin / Northrop Grumman AN/APG-78 Longbow fire-control radar[290] (Note: can only be mounted on the AH-64D/E) ![]() IL-78 Type: Refueling Tanker Specifications: Crew: 6 Capacity: Max 100,000 kg payload (T-6 military jet fuel)[24] Length: 46.59 m (152 ft 10 in) Wingspan: 50.5 m (165 ft 8 in) Height: 14.76 m (48 ft 5 in) Wing area: 300 m2 (3,200 sq ft) Empty weight: 72,000 kg (158,733 lb) Max takeoff weight: 210,000 kg (462,971 lb) Special equipment: 3 x UPAZ-1M 'Sakhalin', (oonifitseerovannyy podvesnoy agregaht zaprahvki — standardised suspended refuelling unit), refuelling pods; Two on pylons under the outer wings, and the third on the port side of the rear fuselage. Fuel transfer rate: 900 to 2,200 liters/min Powerplant: 4 × Aviadvigatel D-30 KP turbofan engines, 118 kN (27,000 lbf) thrust each Performance Maximum speed: 850 km/h (528 mph; 459 kn) Range: 7,300 km (4,536 mi; 3,942 nmi) Service ceiling: 12,000 m (39,370 ft) Thrust/weight: 0.23 ![]() |
![]() ![]() |
![]() ![]() |
Gondor | Apr 8 2016, 12:00 AM Post #4 |
![]()
![]() |
Tanks and Armor used by the Royal Gondorian Army Panther K2 Type: Main Battle Tank Specifications: eight55 t (54 long tons; 61 short tons) LengthOverall: 10.8 m (35 ft 5 in) Chassis : 7.5 metres (24 ft 7 in) Width3.6 metres (11 ft 10 in) Height2.4 metres (7 ft 10 in) Crew3 (commander, gunner, driver) ArmorClassified type of composite armour with ERA and NERA modular add-on armour in addition to soft-kill and hard-kill anti-missile defense systems Main armament 120 mm (4.72 in) 55 caliber smoothbore gun (40 rounds) Secondary armament 1× 12.7×99mm (.50 BMG) K6 heavy machine gun (3,200 rounds) 1× 7.62×51mm NATO coaxial machine gun (12,000 rounds) Engine4-cycle, 12-cylinder water-cooled diesel 1,500 hp (1,100 kW) Power/weight27.2 hp/tonne SuspensionIn-arm Suspension Unit Operational range 450 kilometres (280 mi) SpeedPaved road: 70 km/h (43 mph) Cross country: 50 km/h (31 mph) Acceleration from 0–32 km/h (0–20 mph) in 7 seconds ![]() Namer Type: APC Specifications: Weight60 tonnes[3] Crew3 (commander, driver, RCWS operator) + 9 troops ArmorClassified composite matrix of laminated ceramic-steel-nickel alloy + underlaid reactive armour. Sloped modular design. Main armament Samson RCWS equipped with either 12.7 mm (0.50 in) M2 machine gun, or Mk 19 grenade launcher, or smaller MG. Secondary armament 1 × 7.62 mm (0.300 in) FN MAG MG 1 × 60 mm (2.4 in) external mortar 12 smoke grenades Engine1,200 hp (895 kW) turbocharged diesel engine Power/weight20 hp/ton Payload capacity9 infantrymen[4] SuspensionHelical spring Operational range 500 km (310 mi) Speed60 km/h (40 mph) ![]() BMP-3 Type: IFV Specifications: Weight18.7 tonnes (18.4 long tons; 20.6 short tons) Length7.14 m (23 ft 5 in) Width3.2 m (10 ft 6 in) Height2.4 m (7 ft 10 in) Crew3 (commander, gunner, driver) 7 troopers (+ 2 additional seats) ArmorAluminium alloy + steel, 35mm+ frontally, all around small arms fire protection Main armament 100 mm gun/launcher 2A70 (able to fire shells or the 9M117 Bastion ATGM), 30 mm autocannon 2A72 Secondary armament 3×7.62 mm PKT machine guns EngineUTD-29M diesel 500 hp (375 kW) Power/weight27 hp/tonne Suspensiontorsion bar Operational range 600 km (370 mi) Speed72 km/h (45 mph) (road) 45 km/h (28 mph) (off-road) 10 km/h (6.2 mph) (water) Edited by Gondor, Apr 8 2016, 02:48 AM.
|
![]() ![]() |
![]() ![]() |
Gondor | Apr 11 2016, 02:17 AM Post #5 |
![]()
![]() |
Merkava 4 Crew:4 65 t Length (gun forward) 9 m Hull length 7.6 m Width 3.72 m Height 2.66 m Armament Main gun 120-mm smoothbore ATGW LAHAT ATGM Machine guns 1 x 12.7-mm 2 x 7.62-mm Mortar 1 x 60-mm Elevation range ? Traverse range 360 degrees Ammunition load Main gun 48 rounds ATGW ? Machine guns ? Mobility Engine General Dynamics GD883 V12 diesel Engine power 1 500 hp Maximum road speed > 60 km/h Range 500 km Maneuverability Gradient 60% Side slope 30% Vertical step ~ 1 m Trench ~ 3 m Fording ~ 1.4 m |
![]() ![]() |
![]() ![]() |
1 user reading this topic (1 Guest and 0 Anonymous) |
« Previous Topic · National Factbooks · Next Topic » |