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・ NRING Circuit
・ NRIP1
・ NRIP2
・ Nripa Kama II
・ Nripatindravarman
・ Nripen Chakraborty
・ Nripen Goswami
・ Nripendra Misra
・ Nripendra Narayan
・ Nripendra Narayan Government High School
・ Nripendra Narayan Memorial High School
・ Nripendra Nath Roy
・ Nripjit Singh Bedi
・ Nrisimha Tapaniya Upanishad
・ Nrisingha Prasad Bhaduri
NRIST I-series UAV
・ NRIST II-series UAV
・ NRIST S-100 series UAV
・ NRIST S-200 series UAV
・ NRIST S-300 series UAV
・ NRIST S-70 series UAV
・ NRIST S-80 series UAV
・ NRIST S-series UAV
・ NRIST UAV
・ NRIST Unmanned Helicopters
・ NRIST W-series UAV
・ Nritoday
・ Nritya Creations
・ Nrityagram
・ NRJ


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NRIST I-series UAV : ウィキペディア英語版
NRIST I-series UAV

NRIST I-series UAVs are Chinese UAVs developed by (Nanjing Research Institute of Simulation Technology (南京模拟技术研究所) ) (NRIST), also known as the 60th Research Institute of People's Liberation Army General Staff Department (总参六十所), an ISO 9001 ceritified research/production facility headquartered in Nanjing.
==I-2==
I-2 remotely piloted vehicle is an unmanned rotary wing UAV is in conventional helicopter layout and it has tricyle landing gear. It is primarily intended to be a training aid to air defense crews by simulating combat maneuvors of attack helicopters in combat senarios. In addition to the three-blade main rotor, there is also an two-blade propeller driven tractor engine mounted in the nose, but I-2 lacks any tail rotor. Simulation I-2 unmanned rotary wing UAV performs can also be used in tactic development. Unlike most unmanned helicopters that takes-off on their own, I-2 adopts an unusual way to take-off of catapult assisted take-off: after engine started, the UAV is can be catapulted into the air. In addition to vertical landing, it can also land by taxiing. Specification:〔(【引用サイトリンク】 title=I-series UAVs )
*Rotor diamter (m): 2
*Length (m): 1.7
*Max take-off weight (kg): 12
*Max speed (m/s): 35
*Ceiling (m): 800
*Endurance (h): 1
*Launch: catapult
*Recovery: taxiing
*Max wind scale allowed for operation: 4
*Temperature range (°C): -40 to +50
*Propulsion: CYS-40F

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「NRIST I-series UAV」の詳細全文を読む



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