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The Kingdom of Gondor Armed Forces
Topic Started: Apr 7 2016, 03:41 AM (322 Views)
Gondor
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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

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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

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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.

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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


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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.
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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


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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)

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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)


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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)

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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]

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Edited by Gondor, Apr 7 2016, 03:48 PM.
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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)


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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

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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

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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)

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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.
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Gondor
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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

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