BIRD EYE 650D

อากาศยานไร้คนขับทางยุทธวิธีขนาดเล็ก – SMALL TACTICAL UAS (STUAS)

42003 Birdeye 650D

 

 

 

 

 

 

 

 

 

 

Generral

Advanced long endurance SMALL TACTICAL UAS (STUAS), providing real-time day/night imagery data for urban operation and over-the-hill intelligence.

Main Features and Capabilities

  • Wide coverage, stabilized day/night payload and moving target tracker
  • Multiple payload capability
  • Fully automated and autonomous flight
  • Very low-visual and noise signature
  • Unique safety fail-safe recovery system

Typical Missions

  • Reconnaissance
  • Urban Operation
  • Counter-Terrorism
  • Law Enforcement
  • Patrol and Convoys Escort
  • Radio Relay

Performance

  • Mission Radius: 150 km
  • Endurance: >15 hr
  • Ceiling: >15000 ft
  • Loiter Speed: 40 kts
  • Maximum Speed: 80 kts

Technical Data

  • Maximum Takeoff Weight (MTOW): 30 kg
  • Maximum payload weight for full endurance: 5.5 kg
  • Gasoline fuel engine
  • Wingspan: 4 m

yourfile 650D

HERON TP

อากาศยานไร้นักบินระยะกลาง (MALE UAV SYSTEM)

Maritime-Heron800

 

 

 

 

 

 

 

 

 

 

 

 

ทั่วไป (General)

Medium Altitude Long Endurance (MALE) UAV System sets the new standard in mission envelope payload capability and system reliability.

คุณสมบัติของ Heron TP (The Heron TP Offers):

  • Multi-mission / multi Payload configuration
  • Large internal volume for variety of payloads
  • All weather capability
  • Satellite Communication (SATCOM) for extended range (Beyond Line of SIght – BLOS)
  • Operation above commercial traffic (Up to 45,000 ft)
  • Mission endurance above 30 hours
  • Triple redundant avionics
  • Automatic Taxi-Takeoff-Landing (ATOL system)
  • Certified to STANAG 4671
  • Compatibility with NATO Standards

ข้อมูลทางเทคนิค (Technical Data)

  • น้ำหนักขึ้นบินสูงสุด (Maximal Takeoff Weight): 5400 กิโลกรัม
  • น้ำหนักกล้องสำหรับภารกิจ (Typical Mission Payload): 1000 กิโลกรัม
  • ความยาวปีกรวม (Wingspan): 26 เมตร
  • ความยาวลำตัว (Length): 14 เมตร
  • เครื่องยนต์ PT6 แบบใบพัด ขนาด 1200 แรงม้า (1200 hp PT6 Turboprop Engine)
  • ความเร็วบินสูงสุด (Max speed): 220 น๊อต

“ใช้ประจำการสำหรับปฏิบัติภารกิจอย่างเต็มรูปแบบในกองทัพอากาศอิสราเอล”

“Fully Operational with the Israeli Airforce”

T129

t129-atak-6

The ATAK programme was begun to meet the Turkish Armed Forces’ requirements for an attack and tactical reconnaissance helicopter. Turkey announced on 30 March 2007 that it had decided to negotiate with Agusta Westland to co-develop and produce 51 (with 40 options) attack helicopters based on the Agusta A129 Mangusta. It is to be assembled in Turkey by Turkish Aerospace Industries (TAI) as the T-129. On 7 September 2007

General characteristics:
– Crew: 2 ; pilot and co-pilot/gunner
– Length: 13.45 m (44 ft 1 in)/ Height: 3.4 m (11 ft 2 in)
– Rotor diameter: 11.90 m (39 ft 0 in)
– Disc area: 111.22 sq.m (1,197.25 sq.ft)
– Empty weight: 2,350 kg
– Max. takeoff weight: 5,000 kg (11,023 lb)
– Powerplant: 2 x LHTEC CTS800-4A turboshaft, 1,014 kW (1,361 shp) each
– Propellers: 5-bladed main rotor
Performance:
– Maximum speed: 278 km/h (151 knots, 174 mph)
– Cruise speed: 269 km/h (145 konts, 167 mph)
– Range: 561 km (303 nmi, 341 mi)
– Ferry range: 1,000 km (540 nmi, 620 mi)
– Service ceiling: 6,096 m (20,000 ft)
– Rate of climb: 14.0 m/s (2,750 ft/min)