Vertipedia - Kawasaki MCH-101

Airborne Mine Countermeasures (AMCM) and transportation variant for the Japan Maritime Self Defense Force (JMSDF)

Overview

Data on design, manufacture and status

Design authority: AgustaWestland N.V.

Primary manufacturer: Kawasaki Heavy Industries Ltd.

Parent type: Kawasaki AW101/EH101

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 2 in Side-by-side arrangement

Landing gear: Wheels (all retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Layout and Dimensions

Weights and Performance

Engine Details

Primary Lift Device

Primary Control Device

Overall Dimensions
Overall Height:	6.66 m	21.9 ft
Overall Length:	22.83 m	74.9 ft
Overall Width:	18.59 m	61.0 ft

Airframe Dimensions
Airframe Length:	19.30 m	63.3 ft
Airframe Width:	5.06 m	16.6 ft
Airframe Height:	5.09 m	16.7 ft

Landing Gear Dimensions
Landing Gear Base:	6.99 m	22.9 ft
Landing Gear Track:	3.82 m	12.5 ft

Cabin Dimensions
Cabin Internal Height:	1.83 m	6.0 ft
Cabin Internal Length:	6.50 m	21.3 ft
Cabin Internal Width:	2.49 m	8.2 ft

Weights
Max Gross Weight (ground):	14,600 kg	32,187 lb
Max Gross Weight (airborne):
Max Take-off Weight:	14,600 kg	32,187 lb
Empty Weight:

Climb Performance
Max Rate of Climb:

Hover Performance
Hover Ceiling IGE:	3,307 m	10,850 ft
Hover Ceiling OGE:

Limitations
Max Level Flight Speed:	278 km/h	150 kts
Never Exceed Speed:	309 km/h	167 kts
Service Ceiling:

Range and Endurance
Max Range:	1,360 km	734 nm
Max Endurance:	7 hrs

Provided powerplant data is for uninstalled, sea level, static operations.

Powerplant
Number of engines:	3
Designation:	Turbomeca RTM 322 02/8 Mk250 turbine
Manufacturer:	Turbomeca

Normal Ratings
Max continuous:	1492 kW	2000 hp
Take-off / rated:	1694 kW	2271 hp
Intermediate:	1604 kW	2150 hp
Maximum:

OEI Ratings
OEI contingency:	1791 kW	2401 hp
OEI continuous:
OEI 30-second:
OEI intermediate:

Main Rotor Characteristics
Diameter:	18.59 m	61.00 ft
RPM:
Direction of Rotation:	Counterclockwise
Hub Type:	Fully articulated with elastomeric bearings

Main Rotor Blade Characteristics
Blade Construction:	Glass/carbon with metallic erosion shields
Blade Chord:	0.680 m	2.23 ft
Blade Tip Geometry:	BERP III with anhedral
Blade Twist:
Number of Blades:	5

Main Rotor Derived Characteristics
Disc Area:	271.51 m²	2922.6 ft²
Disc Loading:	53.77 kg/m²	11.014 lb/ft²
Solidity:	0.1164

Main Rotor Blade Derived Characteristics
Blade area per blade:	6.32 m²	68.0 ft²
Tip Speed:

Tail Rotor Characteristics
Diameter:	4.10 m	13.45 ft
Configuration:	Pusher
Direction of Rotation:	Top blade aft
RPM:

Tail Rotor Blade Characteristics
Number of Blades:	4
Blade Construction:	Composite
Blade Chord:
Blade Twist:

Tail Rotor Derived Characteristics
Disc Area:	13.20 m²	142.1 ft²
Solidity:

Tail Rotor Blade Derived Characteristics
Tip Speed:
Blade Area (per blade):

References

References and sources used

Japan’s MCH-101: All Your Mine Are Belong to Us

Defense Industry Daily staff
Defense Industry Daily, 2013, Jun 21
Website

Related VFS Resources

Resources related to the MCH-101 , provided by the Vertical Flight Society.

Forum Proceedings

Vertiflite articles

Enter a search term in the box above.

Web files from vtol.org

Enter a search term in the box above.

Webpages from vtol.org

Enter a search term in the box above.

Images from the VFS Gallery

Enter a search term in the box above.

Refine / filter your search or find more resources

Related Public Resources

Resources related to the MCH-101 , provided by public sources across the internet.

Publicly-funded resources provided by the US Government

Search at NASA Technical Reports Server (NTRS).

Search at Defense Technical Information Center (DTIC).

Search at SciTech Connect (OSTI).

Public resources provided by select scholarly and academic sources

Search at European Rotorcraft Forum Document Repository.

Search at IOPScience.

Search at CiteSeerX.

Additional links

Search for at Google Scholar.

Search for at Bielefeld Academic Search Engine (BASE).

Search for at Semantic Scholar.

Search for at CORE (COnnecting REpositories).

Search for at JSTOR.

Images

Overview

Attribution

Main rotor

Attribution

Main Rotor Diameter:	18.59 m	61.00 ft
Max Gross Weight (ground):	14,600 kg	32,187 lb

Number of engines:	3 Turbines
Max Level Flight Speed:	278 km/h	150 kts
Max Range:	1,360 km	734 nm
Max Endurance:	7 hrs	7 hrs