(･∀･)ｂ　T-50

JA 0 ｡ﾟ( ﾟ^∀^ﾟ)ﾟ栗金 24,538

2009-03-13 07:02

궴궋궯궲귖갂듰뜎뜎럀@궳궼궶궋궳궥귝굸굸

긚긼[귽궳둎뵯뭷궻갂뫮괻괧괧뾭긚긡깑긚먰벉@궳궥갃

긚[긬[긏깑[긛@\븊^뱳괻괧괧귉궻뫮뛕댰렞뼖갲궳궥갃

깓긘귺똓궳궻둎뵯긓[긤궼굍굲|괫괥궻귝궎궳궥궺갃굎|괫괥궼긚긼[귽롊궳궻긓[긤궳궥갃

괧괥괥괱봏룊뷅뛱궴뙻궎궞궴궳궥궔귞갂뜞봏렳@궕뚺둎궠귢귡궔귖궢귢귏궧귪궺괃(^곉^)굚

궩귢궸궢궲귖롰쀞궕뫝궋굸@

굎|괫괥괺걁괷굺괫괥굁걂궼멟릋뾻궻댡귖궇귡귝궎궳궥궕갂궞귢궳궼긇긥[긤궻뼰궋굍굲|괪괯궻귝궎궶갋갋갋굸굸

굎|괫괥`@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@굎|괫괥괶

굎|괫괥괷

굎|괫괥괹

굎|괫괥괺

General characteristics

Crew: 1 (pilot)/2(crew)for Indian variant
Length: 22.0 m (72 ft 2 in)
Wingspan: 14.2 m (46 ft 7 in)
Height: 6.05 m (19 ft 10 in)
Wing area: 78.8 m² (848 ft²)
Empty weight: 18,500 kg (40,786 lb)
Loaded weight: 26,000 kg (57,320 lb)
Useful load: 7,500 kg (16,535 lb)
Max takeoff weight: 37,000 kg (81,571 lb)
Powerplant: 2~ Saturn-Lyulka AL-41F turbofan
- Dry thrust: 96.1 kN (9,800 kgf, 21,605 lbf) each
- Thrust with afterburner: 152 kN (15,500 kgf, 34,172 lbf) each

Performance

Maximum speed: Mach 2+ at altitude (2450+ km/h, 1,500 mph)
g-limits: 9 g)
Cruise speed: 1,300 km/h (807.8 mph)
Ferry range: 4,000 to 5,500 km (2,485 to 3,418 mi)
Service ceiling: 65,000 ft (19,812 m)
Rate of climb: 350 m/s (68,898 ft/min)
Wing loading: 470 kg/m² (96.3 lb/ft²)
Thrust/weight: 0.84 (dry thrust)
Minimum thrust/weight:
- With afterburner: 1.19
Runway length requirement: 350 m (1,148 ft)
Endurance: 3.3 hrs (198 mins)

Armament

Guns: 2~30 mm internal cannon
Hardpoints: 8 total, 4 on each side of the aircraft.

Avionics

Radar: N050(?)BRLS AESA/PESA Radar (Enhancement of IRBIS-E) on SU-35
- Frequency: 3 Cm (0.118 in) (X-band)
- Diameter: 0.7 m (2 ft 4 in)
- Targets: 32 tracked, 8 engaged
- Range: 400 km (248 mi)
  - EPR: 3 m² (32.3 ft²) at 160 km (99.4 mi)
  - RCS: 0.01 m² at 90 km (55 mi)
  - Azimuth: +/-70걢, +90/-50걢
- Power: 4,000 W
- Weight: 65 to 80 kg (143 to 176 lb)

翻訳を見る

(·∀·) b　T-50

그렇다고 해도, 한국 국산기는 아니어요 ww

스호이로 개발중의, 대F22용 스텔스 전투기입니다.

슈퍼 크루즈 기능부여등 F22에의 대항 의식 만만합니다.

러시아군으로의 개발 코드는 Su－50같네요.T－50은 스호이사로의 코드입니다.

2009 연초 비행이라고 하는 것이기 때문에, 금년실기가 공개될지도 모르겠네요♪(^∀^) b

그렇다 치더라도 종류가 많은 w　

T－50 E(Cy50K)는 전진날개의 안도 있는 것 같습니다만, 이것으로는 카너드가 없는 Su－47과 같은···ww

T－50A　　　　　　　　　　　　　　　　　　　　　　　　　　　　　　　T－50B

T－50C

T－50D

T－50E

General characteristics

Crew: 1 (pilot)/2(crew) for Indian variant
Length: 22.0 m (72 ft 2 in)
Wingspan: 14.2 m (46 ft 7 in)
Height: 6.05 m (19 ft 10 in)
Wing area: 78.8 m² (848 ft²)
Empty weight: 18,500 kg (40,786 lb)
Loaded weight: 26,000 kg (57,320 lb)
Useful load: 7,500 kg (16,535 lb)
Max takeoff weight: 37,000 kg (81,571 lb)
Powerplant: 2× Saturn-Lyulka AL-41F turbofan
- Dry thrust: 96.1 kN (9,800 kgf, 21,605 lbf) each
- Thrust with afterburner: 152 kN (15,500 kgf, 34,172 lbf) each

Performance

Maximum speed: Mach 2+ at altitude (2450+ km/h, 1,500 mph)
g-limits: 9 g)
Cruise speed: 1,300 km/h (807.8 mph)
Ferry range: 4,000 to 5,500 km (2,485 to 3,418 mi)
Service ceiling: 65,000 ft (19,812 m)
Rate of climb: 350 m/s (68,898 ft/min)
Wing loading: 470 kg/m² (96.3 lb/ft²)
Thrust/weight: 0.84 (dry thrust)
Minimum thrust/weight:
- With afterburner: 1.19
Runway length requirement: 350 m (1,148 ft)
Endurance: 3.3 hrs (198 mins)

Armament

Guns: 2×30 mm internal cannon
Hardpoints: 8 total, 4 on each side of the aircraft.

Avionics

Radar: N050(?) BRLS AESA/PESA Radar (Enhancement of IRBIS-E) on SU-35
- Frequency: 3 Cm (0.118 in) (X-band)
- Diameter: 0.7 m (2 ft 4 in)
- Targets: 32 tracked, 8 engaged
- Range: 400 km (248 mi)
  - EPR: 3 m² (32.3 ft²) at 160 km (99.4 mi)
  - RCS: 0.01 m² at 90 km (55 mi)
  - Azimuth: +/-70о, +90/-50о
- Power: 4,000 W
- Weight: 65 to 80 kg (143 to 176 lb)

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(･∀･)ｂ T-50

(·∀·) b T-50

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(･∀･)ｂ　T-50

(·∀·) b　T-50