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OH-1 Japanese Light Scout and Observation Helicopter

OH-1

Attack Helicopter
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Basic Information
Name
OH-1 Japanese Light Scout and Observation Helicopter
Designation
OH-1
Alternate Designation
Kawasaki OH-1 Japanese Light Scout and Observation Helicopter
Equipment Type
Attack Helicopter
Manufacturer
Kawasaki
Date of Introduction
2000
Description

The Kawasaki OH-1 (nickname: "Ninja") is a military scout/observation helicopter developed and manufactured by the Kawasaki Aerospace Company. The primary operator is the Japan Ground Self-Defense Force (JGSDF), who originally procured the OH-1 as a domestically-produced successor to their existing OH-6D Loach fleet. The OH-1 has the distinction of being the first helicopter to be entirely produced in Japan. In addition to its use an observation helicopter, it can also be armed with various munitions to directly participate in combat; such weapons include a limited quantity of anti-tank missiles or air-to-air missiles for self-defense purposes. Several variants of the OH-1 have been proposed, these have included derivatives of the type to serve as an attack helicopter as well as an aborted project to develop utility helicopter based on OH-1. As of March 2014, a total of 38 OH-1s have entered service with the JGSDF, so far these have complemented the existing OH-6Ds rather than replace them.

Air & Air Defense Specifications
Crew 2
Engine Turboshaft (888 hp)
Max Speed 306.0 km/h
Range 550.0 km
Variants
AH-2 Proposed attack helicopter derivative that would have featured uprated engines and additional anti-tank armaments; rejected in favour of Boeing AH-64 Apache.
UH-X utility helicopter Technology developed by Kawasaki for the OH-1 is being integrated into a new aircraft design, the UH-X , in order to "reduce technological risks associated with development and appropriately control life cycle costs," according to the company. The new aircraft is expected by 2017, according to a Shephard Media release dated May 29, 2012. Kawasaki has proposed a new cabin, transmission, avionics and engines for the utility version, including a new control system, rotor hub and enhanced rotor-blade transmission protection. In fiscal year 2006, Tokyo began funding development of a more powerful engine (with a goal of 1,300 shp). More than 120 helicopters are needed to meet the JGSDF requirement for a utility helicopter. Fuji Heavy Industries was selected as prime contractor for the UH-X helicopter program in July 2015. The aircraft will be based on the Bell 412 twin-engine utility helicopter.
System
Alternative Designation Kawasaki OH-1 Japanese Light Scout and Observation Helicopter
Type Attack Helicopter
Primary Function Reconnaissance missions, Ground attack and Close-Air Support
Manufacturer Kawasaki
Crew 2 ea
Blades, Main Rotor 4 ea
Number of Engines 2 ea
Main rotor diameter 11.6 m
Main rotor area 1138 ft
Tail Rotor, Name Fenestron (fantail) tail rotor
Blades, Tail Rotor 8-18 ea
Number of Hard Points Hardpoints: 4 × pylons for rockets, gun pods, anti-tank missiles, or Type 91 air-to-air missiles
Note #1: Each crew member has two LCD colour multi-function displays, and the gunner has a head-up display. The mission avionics include a trainable roof-mounted Kawasaki package (forward of the main rotor) with a Fujitsu thermal imager, NEC colour TV camera and NEC laser rangefinder. Protection is enhanced by the installation of an infra-red jammer on the helicopter's spine to rear of the main gearbox.
Dimensions
Length 12 m
Width INA
Main Rotor Diameter 11.6 m
Weight, Combat 3550 kg
Weight, Empty 2500 kg
Weight, Gross 4000 kg
Height 3.8 m
Automotive
Engine Name 2 x Mitsubishi TS1-M-10
Engine Type Turboshaft
Engine Power 888 hp
Cruising Range 550 km
Speed, Maximum 306 km/h
Speed, Average INA
Maximum Altitude 5000 m
Main Gun System
Hardpoints Hardpoints: 4 × pylons for rockets, gun pods, anti-tank missiles, or Type 91 air-to-air missiles
Missile Weapon Systems
Missile System #1
Name Toshiba Type 91 short-range air-to-air missiles, anti-tank missiles
Type Air to Air and Anti-tank Missiles
Length 1.43 m
Weight 11.5 kg
Diameter 80 mm
Engine Solid Rocket Motor Mach 1.9
Guidance System Infrared homing
Fire Control and Avionics
Fire Control System Type INA
Fire Control Radar INA
Navigation Radar INA
Digital or Analog Cockpit Digital Cockpit
Direct Fire Control INA
Laser Designator INA
Protection
Add on Armor Cockpit is fitted with armor protection
Stealth Properties INA
Heat Signature Reduction INA
NBC Protection INA
EW Counter Measures/CCM INA
Counter Measures (Chaff/Flares) Infra-red jammer on the helicopter's spine to rear of the main gearbox. Used to jam IR homing missile sensors.
Details
Country of Origin Japan
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Filter Label
O
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
12 m
Width
Height
3.8 m
Weight
3550 kg
Operators (1)
Japan
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