JJSmithJr
Senior
- Jul 1, 2018
- 924
Land Equipment:
Air Equipment:
Equipment | Type | Specifications | Price |
BTR-94 | Armored Personnel Carrier | Main armament: twin 23x152mm 2A7M cannon Secondary armament: 7.62 mm PKT machine gun Engine: diesel engine 300 hp Ground clearance: 475 mm Fuel capacity: 300 litres Operational range: 600 km Speed: 85 km/h, 9 km/h swim | $630,000.00 |
KraZ-6322 | Logistics Truck | Engine: YaMZ 238DE2 14.86 L 8 cyl turbodiesel Power: 330 PS (243 kW) /2400rpm Torque: 1225Nm /1225rpm Top speed: 75 mph | $150,000.00 |
T-84 | Main Battle Tank | Armour: Steel, composite, ERA Main armament: 125 mm smoothbore KBA-3 cannon (43 rds) Secondary armament: 7.62 mm KT-7.62 Coaxial machine gun 12.7 mm KT-12.7 anti-aircraft machine gun Engine: KMDB 6TD-2 6-cylinder diesel 1,200 hp (890 kW) Power/weight: 26 hp/tonne Suspension: Torsion-bars, hydraulic dampers Ground clearance: 0.515 m (1 ft 8.3 in) Fuel capacity:1,300 l (290 imp gal; 340 US gal) Operational range: 540 km (340 mi) Speed: 65 km/h (40 mph) – 70 km/h (43 mph) | $4,250,000.00 |
T-64BM2 | Light Battle Tank | Armour: Glass-reinforced plastic sandwiched between layers of steel. ERA plates optional Main armament: D-81T (aka 2A46)125 mm smoothbore gun Secondary armament: 7.62 mm PKMT coaxial machine gun, 12.7 mm NSVT anti-aircraft machine gun Engine: 5TDF 5-cylinder diesel 700 hp (522 kW) Power/weight: 18.4 hp/tonne (13.7 kW/ton) Suspension: Torsion bar Operational range: 500 km (310 mi), 700 km (430 mi) with external tanks Speed: 45–60 km/h (28–37 mph) | $1,750,000.00 |
Kolchuga passive sensor | Passive Aircraft Sensor | 
Kolchuga passive sensor - Wikipedia | $44,000,000.00 |
Air Equipment:
Equipment | Type | Specifications | Price |
Antonov An-140 | Regional Airliner/Airlifter | Crew: 2 Capacity: 52 pax / 6,000 kg (13,228 lb) max payload Length: 22.605 m (74 ft 2 in) Wingspan: 24.505 m (80 ft 5 in) Height: 8.225 m (27 ft 0 in) Wing area: 51 m2 (550 sq ft) Empty weight: 12,810 kg (28,241 lb) Max takeoff weight: 19,150 kg (42,219 lb) Maximum zero fuel weight: 17,800 kg (39,242 lb) Maximum landing weight: 19,100 kg (42,108 lb) Fuel capacity: 4,370 kg (9,634 lb) Powerplant: 2 × Motor-Sich AI-30 series 1 turboprop engines, 1,838 kW (2,465 hp) each (licence-built Klimov TV3-117VMA-SBM1) Alternate engines: 2x Pratt & Whitney Canada PW127A turboprops driving Hamilton Sundstrand 247F propellers Propellers: 6-bladed Aerosyla Stupino SV-14, 3.6 m (11 ft 10 in) diameter constant-speed fully feathering reversible propellers Performance Cruise speed: 575 km/h (357 mph, 310 kn) at 7,200–7,500 m (23,622–24,606 ft) max Economical cruise speed: 520 km/h (320 mph; 280 kn) at 7,200–7,500 m (23,622–24,606 ft) Range: 900 km (560 mi, 490 nmi) with 6,000 kg (13,228 lb) payload at econ. cruise 2,100 km (1,300 mi; 1,100 nmi) with 52 pax 3,700 km (2,300 mi; 2,000 nmi) with 33 pax Service ceiling: 7,600 m (24,900 ft) Rate of climb: 6.83 m/s (1,344 ft/min) Power/mass: 0.19194 kW/kg (0.11675 hp/lb) Balanced field length: 1,350 m (4,429 ft) | $15,000,000.00 |
Antonov 70 | Strategic Airlifter | Crew: 3-4 flight crew (two pilots and flight engineer (optional navigator)) + loadmasters and cargo attendants Capacity: 300 troops or 206 stretcher cases / 47,000 kg (103,617 lb) max payload Length: 40.73 m (133 ft 8 in) Wingspan: 44.06 m (144 ft 7 in) Height: 16.38 m (53 ft 9 in) Airfoil: TsAGI P-202[67] Empty weight: 66,230 kg (146,012 lb) Max takeoff weight: 145,000 kg (319,670 lb) Powerplant: 4 × Progress D-27 turboprop, 10,350 kW (13,880 hp) each Propellers: 14-bladed Aerosyla Stupino SV-27, 4.5 m (14 ft 9 in) diameter contra-rotating propeller (8-bladed forward ; 6-bladed rear) Performance Maximum speed: 780 km/h (480 mph, 420 kn) Cruise speed: 750 km/h (470 mph, 400 kn) at 9,100–11,000 m (29,856–36,089 ft) 800 km/h (500 mph; 430 kn) max Stall speed: 113 km/h (70 mph, 61 kn) Range: 1,350 km (840 mi, 730 nmi) with 47,000 kg (103,617 lb) payload from 1,800 m (5,906 ft) runway 3,800 km (2,400 mi; 2,100 nmi) with 38,000 kg (83,776 lb) payload from 1,800 m (5,906 ft) runway 5,000 km (3,100 mi; 2,700 nmi) with 30,000 kg (66,139 lb) payload from 1,800 m (5,906 ft) runway 7,400 km (4,600 mi; 4,000 nmi) with 20,000 kg (44,092 lb) payload from 1,800 m (5,906 ft) runway 8,000 km (5,000 mi; 4,300 nmi) with maximum fuel from 1,800 m (5,906 ft) runway (STOL operations with reduced range) Service ceiling: 12,000 m (39,000 ft) Rate of climb: 24.9 m/s (4,900 ft/min) Power/mass: 0.316 kW/kg (0.192 hp/lb) max Take-off field length: 1,800 m (5,906 ft) Landing field length: 2,000 m (6,562 ft) Take-off run STOL 30,000 kg (66,139 lb) payload: 600 m (1,969 ft) Take-off run STOL 35,000 kg (77,162 lb) payload: 915 m (3,002 ft) | $120,000,000.00 |
