超级军网土耳其宇航工业公司研制的无人机TIHA！
来源：百度文库 编辑：超级军网 时间：2024/04/28 05:19:17
Program Definition:
The TIHA, Turkish Indigenous MALE (Medium Altitude Long Endurance) Unmanned Aerial Vehicle (UAV) System Program signed between the Undersecretariat for National Defense (SSM) and TAI at December 24, 2004 to meet the MALE UAV requirements of Turkish Armed Forces (TAF). Program covers design, development, production, test and delivery of three air vehicle prototypes, all related ground systems and technical documentation, consist of "Conceptual Design", "Preliminary Design", "Detail Design and Development" and "Tests and Evaluation" phases. During the development phase, a Systems Integration Laboratory (SIL), where system elements and their interfaces will be developed and integrated is established. Consequently, the TIHA System,
System Definition:
With TIHA system, which is developed for day and night real time image intelligence for surveillance, reconnaissance, fixed/moving target detection, identification and tracking missions; the following payload can be carried on board:
Electro-Optical Day Camera (EO Day TV),
Day Camera (EO-Electro Optic) / Thermal Camera (IR-Infrared) / LRF-Laser Range Finder & LD-Laser Designator and Spotter,
SAR-Synthetic Aperture Radar / MTI- Moving Target Indicator & ISAR-Inverse SAR.
Full composite airframe is composed of monocock fuselage, detachable wing and V-Tail, retractable landing gear, equipment bays, service doors and other structural components. The air vehicle is powered by a pusher type piston-prop propulsion system. The airframe is equipped with miscellaneous sub systems like fuel system; de/anti-ice devices; environmental conditioning system for cooling/heating requirements of the compartments.
The avionics system includes a Flight Management System (FMS); integrated to FMS, flight sensors (pitot-static sensor, embedded GPS/INS, magnetic heading, displacement, temperature, pressure transducers), actuators; dedicated communication and identification devices; mission control, record; and other control and interface units.
Technical Specifications:
TIHA system basic performance parameters are as follows:
Service Ceiling: 30,000 ft
Endurance: 24 hrs
Cruise Speed: >75 kts
Environmental Conditions: 15 kts side wind, 20 kts head wind; temperature, humidity, rain and icing limits as defined in MIL-HDBK-310
The TIHA, Turkish Indigenous MALE (Medium Altitude Long Endurance) Unmanned Aerial Vehicle (UAV) System Program signed between the Undersecretariat for National Defense (SSM) and TAI at December 24, 2004 to meet the MALE UAV requirements of Turkish Armed Forces (TAF). Program covers design, development, production, test and delivery of three air vehicle prototypes, all related ground systems and technical documentation, consist of "Conceptual Design", "Preliminary Design", "Detail Design and Development" and "Tests and Evaluation" phases. During the development phase, a Systems Integration Laboratory (SIL), where system elements and their interfaces will be developed and integrated is established. Consequently, the TIHA System,
System Definition:
With TIHA system, which is developed for day and night real time image intelligence for surveillance, reconnaissance, fixed/moving target detection, identification and tracking missions; the following payload can be carried on board:
Electro-Optical Day Camera (EO Day TV),
Day Camera (EO-Electro Optic) / Thermal Camera (IR-Infrared) / LRF-Laser Range Finder & LD-Laser Designator and Spotter,
SAR-Synthetic Aperture Radar / MTI- Moving Target Indicator & ISAR-Inverse SAR.
Full composite airframe is composed of monocock fuselage, detachable wing and V-Tail, retractable landing gear, equipment bays, service doors and other structural components. The air vehicle is powered by a pusher type piston-prop propulsion system. The airframe is equipped with miscellaneous sub systems like fuel system; de/anti-ice devices; environmental conditioning system for cooling/heating requirements of the compartments.
The avionics system includes a Flight Management System (FMS); integrated to FMS, flight sensors (pitot-static sensor, embedded GPS/INS, magnetic heading, displacement, temperature, pressure transducers), actuators; dedicated communication and identification devices; mission control, record; and other control and interface units.
Technical Specifications:
TIHA system basic performance parameters are as follows:
Service Ceiling: 30,000 ft
Endurance: 24 hrs
Cruise Speed: >75 kts
Environmental Conditions: 15 kts side wind, 20 kts head wind; temperature, humidity, rain and icing limits as defined in MIL-HDBK-310
The TIHA, Turkish Indigenous MALE (Medium Altitude Long Endurance) Unmanned Aerial Vehicle (UAV) System Program signed between the Undersecretariat for National Defense (SSM) and TAI at December 24, 2004 to meet the MALE UAV requirements of Turkish Armed Forces (TAF). Program covers design, development, production, test and delivery of three air vehicle prototypes, all related ground systems and technical documentation, consist of "Conceptual Design", "Preliminary Design", "Detail Design and Development" and "Tests and Evaluation" phases. During the development phase, a Systems Integration Laboratory (SIL), where system elements and their interfaces will be developed and integrated is established. Consequently, the TIHA System,
System Definition:
With TIHA system, which is developed for day and night real time image intelligence for surveillance, reconnaissance, fixed/moving target detection, identification and tracking missions; the following payload can be carried on board:
Electro-Optical Day Camera (EO Day TV),
Day Camera (EO-Electro Optic) / Thermal Camera (IR-Infrared) / LRF-Laser Range Finder & LD-Laser Designator and Spotter,
SAR-Synthetic Aperture Radar / MTI- Moving Target Indicator & ISAR-Inverse SAR.
Full composite airframe is composed of monocock fuselage, detachable wing and V-Tail, retractable landing gear, equipment bays, service doors and other structural components. The air vehicle is powered by a pusher type piston-prop propulsion system. The airframe is equipped with miscellaneous sub systems like fuel system; de/anti-ice devices; environmental conditioning system for cooling/heating requirements of the compartments.
The avionics system includes a Flight Management System (FMS); integrated to FMS, flight sensors (pitot-static sensor, embedded GPS/INS, magnetic heading, displacement, temperature, pressure transducers), actuators; dedicated communication and identification devices; mission control, record; and other control and interface units.
Technical Specifications:
TIHA system basic performance parameters are as follows:
Service Ceiling: 30,000 ft
Endurance: 24 hrs
Cruise Speed: >75 kts
Environmental Conditions: 15 kts side wind, 20 kts head wind; temperature, humidity, rain and icing limits as defined in MIL-HDBK-310
The TIHA, Turkish Indigenous MALE (Medium Altitude Long Endurance) Unmanned Aerial Vehicle (UAV) System Program signed between the Undersecretariat for National Defense (SSM) and TAI at December 24, 2004 to meet the MALE UAV requirements of Turkish Armed Forces (TAF). Program covers design, development, production, test and delivery of three air vehicle prototypes, all related ground systems and technical documentation, consist of "Conceptual Design", "Preliminary Design", "Detail Design and Development" and "Tests and Evaluation" phases. During the development phase, a Systems Integration Laboratory (SIL), where system elements and their interfaces will be developed and integrated is established. Consequently, the TIHA System,
System Definition:
With TIHA system, which is developed for day and night real time image intelligence for surveillance, reconnaissance, fixed/moving target detection, identification and tracking missions; the following payload can be carried on board:
Electro-Optical Day Camera (EO Day TV),
Day Camera (EO-Electro Optic) / Thermal Camera (IR-Infrared) / LRF-Laser Range Finder & LD-Laser Designator and Spotter,
SAR-Synthetic Aperture Radar / MTI- Moving Target Indicator & ISAR-Inverse SAR.
Full composite airframe is composed of monocock fuselage, detachable wing and V-Tail, retractable landing gear, equipment bays, service doors and other structural components. The air vehicle is powered by a pusher type piston-prop propulsion system. The airframe is equipped with miscellaneous sub systems like fuel system; de/anti-ice devices; environmental conditioning system for cooling/heating requirements of the compartments.
The avionics system includes a Flight Management System (FMS); integrated to FMS, flight sensors (pitot-static sensor, embedded GPS/INS, magnetic heading, displacement, temperature, pressure transducers), actuators; dedicated communication and identification devices; mission control, record; and other control and interface units.
Technical Specifications:
TIHA system basic performance parameters are as follows:
Service Ceiling: 30,000 ft
Endurance: 24 hrs
Cruise Speed: >75 kts
Environmental Conditions: 15 kts side wind, 20 kts head wind; temperature, humidity, rain and icing limits as defined in MIL-HDBK-310
Air vehicle's basic specifications are:
Property Unit Value
Fuselage Length m 10
Wing Span m 17
Wing Area m 213.6
Wing Aspect Ratio - 22
Wing Sweep (quarter chord) ° 0
MTOW-Maximum Take-off Weight kg 1,500
Fuel Weight kg 250
Payload Weight kg 200
Property Unit Value
Fuselage Length m 10
Wing Span m 17
Wing Area m 213.6
Wing Aspect Ratio - 22
Wing Sweep (quarter chord) ° 0
MTOW-Maximum Take-off Weight kg 1,500
Fuel Weight kg 250
Payload Weight kg 200
土耳其 版 捕食者。。
应该是土版收割者，捕食者是倒V尾
不知道这方面有没有和tb进行军事合作
土鸡有这实力?怕是...
土耳其在航空方面不算弱者啊
而且他找强者合作也容易
而且他找强者合作也容易
不错，挺好看:D
TIHA？太行？？
全阿拉伯鹰·
htucd 发表于 2010-7-17 11:47 
土耳其跟阿拉伯可不是一回事
或者可以说是对立的
伊朗也不是阿拉伯国家
土耳其跟阿拉伯可不是一回事
或者可以说是对立的
伊朗也不是阿拉伯国家
这年头，是个国家就能搞JJ
ssizz 发表于 2010-7-17 12:16
那么“全中东鹰”如何？:D
那么“全中东鹰”如何？:D
htucd 发表于 2010-7-17 19:05
土耳其那地方叫 近东
土耳其那地方叫 近东
ssizz 发表于 2010-7-17 23:28
那么该叫它“全”什么“鹰”啊~~{:yi:}
那么该叫它“全”什么“鹰”啊~~{:yi:}
不如收割者大气
htucd 发表于 2010-7-17 23:38
全土耳其火鸡
全土耳其火鸡
据"中国时报"21日援引日本《读卖新闻》报道，这项消息显示，HTV将取代行将退出宇航任务的航天飞机，全球最大的宇航任务机构NASA给予日本航天研发技术高度的肯定。
tai=ta i=他2，这名字好听 给自己的飞机起这么个好名字
可不要骂我媚外，怎么看着比俺们的全村鹰顺眼？
Flanker-D 发表于 2010-7-17 23:53
呵呵。。。{:hao:}
呵呵。。。{:hao:}
合作还是自己弄的？
LZ，转贴要上地址
未定名 发表于 2010-7-22 20:43
我不记得地址了，抱歉！
我不记得地址了，抱歉！
不咋样吧
外形不错啊，工艺看起来也不差。
都流行把发动机装在机身上方两个倾斜尾翼中间，好处是啥？有利于隐身？
peopletx 发表于 2010-7-30 23:07
抑制红外特征吧？
抑制红外特征吧？
工艺不错。。其他一般
小学都没毕业 ，看不懂
在巴基斯坦论坛上看过， 为之一震， 土耳其现在也挺厉害的了