A flexible and versatile special mission surveillance …tangentlink.com/wp-content/uploads/2013/09/2.-Meeting...5 RUAG Aviation 12.09.2013 Dornier 228 New Generation State-of-the-art

A flexible and versatile special mission

surveillance platform

DORNIER 228 NEW GENERATION

David A Jones General Manager RUAG Aviation Malaysia September 2013

Aviation Defence Space Technology Ammotec

The RUAG Group

12.09.2013 RUAG Aviation 2 |

7’800 employees

Turnover of ~US$2bn

Operations: Switzerland, Germany, Austria, Hungary, Sweden, Australia, Malaysia

Headquarters: Berne/Switzerland

12.09.2013 RUAG Aviation 3

RUAG Aviation – providing total solutions

Aircraft and Component MRO

Program Management and

Upgrades

Engineering

• Maintenance / System

• Fatigue

• Design

Prototyping / Testing / Qualification

Configuration Management

Supply Chain Management

Publications and Training

Ground Support Systems

RUAG – Extensive MRO Capability

Avionics overhaul Cockpit upgrades Starter Generators

Rescue Hoists Turbine Engines Accessory overhaul

Established calibration capability

Establish starter generator capability

Focus on civil light fixed wing and rotary wing

markets

Government – Police, Fire Service, Coastguard

Other civil rotary wing and fixed wing operators

Military organisations

Develop additional services to meet market need

Offer line support for rescue hoists, spares and tooling

Other component support services under review

Support Dornier Do228NG in region

RUAG Aviation Malaysia

12.09.2013 │RUAG Aviation│ 5

Dornier 228 New Generation

State-of-the-art

Glass Cockpit

Honeywell TPE331-10 Up to 7,000 hrs TBO, FAA STC

New 5-bladed Propeller MT-Propeller

RUAG Aviation 6 |

> 300 other improvements

Dornier 228 New Generation – Prepared for the future!

• Mission Performance

Cover maximum possible area in the minimum of time

Extended endurance (>9 hours). Extended range. High max cruise speed (240 KTAS)

• Maneuverability/Flexibility

Ability to monitor targets with pilot confidence

Low stall speed (67 KTAS). Full aileron control even at high AOA. Higher propeller braking for faster controlled descents

• Engine and Field Performance

Able to perform across differing terrains

Take off from unpaved airfields. Engine flat rated to ISA+30°C/86°F at sea level.

• Efficiency

Aerodynamic, with low fuel burn

Generates high lift with 30% lower drag. Fuel burn less than 200kg / search hour) with lowest CO2 emission in its class

• Cockpit and Communication

Fully integrated cockpit

Important features for a surveillance platform

7 | RUAG Aviation

• Visibility

Full and unobstructed view for pilots and operators

• Reliability

Greater than 99% operational reliability

• Direct Maintenance Cost

Low maintenance manhours per flight hour, high engine TBO

• Ease of integration of Mission Systems

Unpressurised fuselage, good ground clearance, optimal fuselage cross section

• Flight Safety State of the art systems (MMS, TAWS overlay, TCAS, Digital Autopilot…). Instantaneous engine power

response for safer STOL operation

Important features for a surveillance platform

8 | RUAG Aviation

• Renowned short-field performance

• Renowned hot and high performance

• Unprepared airfields

• Excellent handling.

• Proven reliability

• Efficient and productive

• High payload transport

• Only aircraft in production in its

performance class (FAR23 commuter <

19.000lbs)


Dornier 228 New Generation Versatile multirole aircraft

Tensing-Hillary Airport (9100 ft) Lukla, Nepal

Unprepared airfield operation, Nigeria

//upload.wikimedia.org/wikipedia/commons/b/bc/Lukla_2001_a.jpg


Dornier 228 New Generation Mission Endurance

Distance Airfield to Search Area (NM)

Searc

h T

ime (

Ho

urs

)

0 100 200 300 400 500 600 700 800 900

9

8

7

6

5

4

3

2

1

0

Distance Airfield to Search Area (NM)

0 100 200 300 400 500 600 700 800 900

1000

900

800

700

600

500

400

300

200

100

0

Searc

h A

rea 1

000 N

M3

Transit to Search Area

•Field Elevation 250 ft Delta ISA 0°C

•Climb with Best Climb Rate to FL 100

•Max Range Cruise Speed

•Wind 0 Kts, Descent Max Range

Search in the Area

• Delta ISA 0°C

• Search Altitude 4000 ft

• Max Endurance Speed

• Sensor Range (both sides) 40 NM

Transit back from Search Area

• Delta ISA 0°C

• Climb with Best Climb Rate to FL 100

• Max Range Cruise Speed

• Wind 0 Kts, Field Elevation 250 ft

MTOW 6675 kg

OWE 3900 kg

Mis. E. 600 kg

Fuel 2250 kg

0

250

500

750

1000

1250

1500

1750

2000

2250

0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400

Range (NM)

Pa

ylo

ad

(kg

)

Dornier 228 New Generation DHC6-400

Payload (kg)/Range (NM) – 100% Load Factor (LF), max Range

19 Pax with 93 kg each

(100% LF)

312 120

Payload –Range


Versatility Quick change troop layout


Fwd Baggage Compartment

Aft Baggage Compartment

Troopers Lightweight Seat

Roller Door

WX Radar

Ladder Stowage Anchorline Cable

Emergency Exits

Special Operations Platform Multirole layout – 2 Operators, 1 Observer, 1 SAR Operator


FWD Baggage Compartment

ATF Baggage Compartment

WX Radar

PBE

Data Master Unit

SLAR

Pax Seat (moveable)

Ladder

Operator Console

Operator Seat

VIS Line Scanner

MWR

Cabin Heater

Roller Door

Oil Spill Sampling Buoy

Pax Seat (moveable)

First Aid Kit Fire Extinguisher

Life

Raft

EO/IR Cabin Heater

Operator Console

Operator Seat

PBE SLAR

Emergency Exits

Special Operations Platform Multirole layout – 1 Operator, 8 Passenger Seats, Toilet

12.09.2013

RUAG Aviation 14 |

FWD Baggage Compartment

ATF Baggage Compartment

WX Radar

Aft facing Pax Seats

Operator Console

Operator Seat

Lavatory

Emergency Exits

Versatility Quick change MedEvac layout (up to 6 double stretchers)

Up to 3 quick change Double Stretchers:

•4 side-facing seats

•3 Pax seats


Fwd Baggage Compartment

Aft Baggage Compartment

WX Radar

Stretcher Stretcher

4 Sideways facing folding Seats

Forwards facing PAX Seats Lavatory

Emergency Exits

EO/IR Pointer MWR

IR/UV Scanner

SLAR Antenna

Surveillance Radar

VIS Scanner

Data link

• LOS Data Links

• BLOS Data Links

• TVDL

• ARC-210, ARC-231

• IFF

• P-25 Radios

• ASE

Avionics Systems

• 2nd FMS

• NVG Compatibility

• Mission Display

• Encrypted Comms

• TACAN

Mission Systems

• General Atomics

• SELEX

• ForceX

• Avalex

• MEDUSA

Sensors and Mission Systems

Special Operations Platform

High ground clearance for sensor installation (0.76m)

High wing - excellent down view through bubble window

Electronic library of (land) targets

Moving Target Identification (MTI)

Data recording and data link

Detection/Highlighting of man-made objects

Sensor Management and cross cue capability

Mission Management System (MMS)

Primary Sensor: Synthetic Aperture Radar (SAR)

Secondary Sensor: EO/IR

Other Equipment: Tactical Radio/Nav Aids, NGV

Compatibility, Search Light, Laser

Illuminator


Police ISR Requirements

EO / IR Search Radar

• Side Looking Airborne Radar (SLAR)

• 360° Surveillance / Search radar (SAR)

• Forward Looking Infrared (FLIR)

• Electro-Optical / Infrared Camera (EO / IR)

• VIS Line scanner

• UV / IR Scanner equipment

• Video camera

• Laser illuminator, Search light

• MWR microwave radiometer

• Direct / Indirect data links

• AIS Airborne/ELR Receiver

• SatCom

• Tactical radio and navigation aids (e.g.

TACAN, Encrypted Communication)

• Mission management systems


Special Operations Platform Sensors and Mission Systems

360° Search Radar

SAR imagery

360° scan or sector scan. Primary sensor for

all search task (except oil spill search)

Max range 200 NM

Small target (periscope, small boats,

life rafts), high sea state range ~ 60 NM

Pulse compression

Moving Target Indication (MTI)

Weight: 35 – 100 kg

Different Suppliers

Search/Surveillance Radar (SAR)


EO / IR

IR / EO imagery

Up to 9 sensors, HD resolution

Typical sensor equipment

Thermal imager

Multi-spectral HD zoom camera

Multi-spectral HD spotter

Laser illuminator, laser pointer

Mission awareness positioning system

Stabilized system, auto-tracking, layover mode

System weight 40 kg to 55 kg

Different Suppliers

Electro Optical / Infrared (EO/IR)


EO / IR

IR / EO imagery

Search Radar

SAR imagery

Cross Cueing capabilities

Workstation sensor calibration

Best identification through combination of

Long range, all weather, broad area radar surveillance (SAR)

Short range, high resolution EO/IR imagery

Cross cueing sensor software available

System weight: 70 – 150 kg

EO/IR + SAR = Optimal Sensor Package


Special Mission Version Delivered

Customer

Air Border Patrol

Coast Guard

Indian Navy

DLR

Finnish Frontier Guard

National Carthogr. Center

Fr Aviation

German Government

Kustwacht

Royal Thai Navy

German Government

Bangladesh Navy


Country

Nigeria

India

India

Germany

Finland

Iran

UK

Germany

Netherlands

Thailand

Germany

Bangladesh

A/C

5

20

30

2

2

4

3

2

2

7

2

2

Mission

Air Border Patrol

Maritime Patrol, SAR

Maritime Patrol

Environmental Prot.

Air Border Patrol

Carthography

Fisheries Patrol

Pollution Surveillance



Pollution Surveillance

Maritime Patrol

Primary Sensor

FLIR, SLOS Camera

360° Radar

360° Radar

Air Data Sensors

360° Radar, SLAR, FLIR

Zeiss Analog Camera

360° Radar

SLAR, IR/UV

360° Radar, SLAR, FLIR

360° Radar

SLAR, IR/UV

360° Radar

Thank you for your attention!


Max. Take-off Weight

Optional (military only)

Max. Landing Weight

optional

Max. Zero Fuel Weight

Operating Weight Empty

Max. Structural Payload

Typical Payload (19 Pax) 93 kg

Fuel at max. Pax

12.09.2013 RUAG Aerospace Services GmbH 24 |

lb

14,109

14,550

13,448

14,109

13,095

8,816

4,279

3,895

1,464

kg

6,400

6,575

6,100

6,400

5,940

3,999

1,941

1,767

664

6.29 m

(20 ft 8 in) 16.56 m

(54 ft 4 in)

16.97 m

(55 ft 8 in)

3.30 m

(10 ft 10 in)

2.54 m (8 ft 4 in)

1.17 m (4 ft 2 in)

• Four (4) 8.9 inch liquid crystal HD

displays

• Navigation display with TAWS overlay,

• Special Mission Operations FMS

available

• Avionic system modifiable. Interface

between mission system and cockpit

avionic possible

• Charts and airport diagrams (optional)

• Checklist (optional)

• Moving Map (optional)

Designed for increased situational

and flight safety awareness


Dornier 228 New Generation 4-tube Universal glass cockpit

Avionics

• EFIS: 2 each PFD’s and MFD’s

• FMS

• ESIS

• TAWS*, TCAS*

• Weather Radar*

• Autopilot*

• HF Radio*

• MMS *

* optional


Engine

Performance

Cabin


671 m

793 m

747 m

450 m

1,870 ft/min

440 ft/min

444 km/h

833 km

7.08 m

1.55 m

2,200 ft

2,600 ft

2,450 ft

1,480 ft

240 KTAS

450 NM

23.23 ft

5.09 ft

Garrett TPE 331-10GP-511D 2 x 776 SHP

(flat rated to ISA + 15°C/59°F) Cruise Fuel Flow 252 lb/h/engine

Take-off Run (1-engine)*

Take-off Distance (1-engine)*

Acc. Stop Distance*

Landing Distance**

Climb, 2 engines*

Climb, 1 engine*

Max. Cruise Speed (10,000 ft)*

Range (Max. Cruise Speed)***

Length

Height

* Max. Take-off Weight, ISA, Sea Level ** Max. Landing Weight, ISA, Sea Level

*** 19 Pax, 85 kg/187 lbs each, 45 min hold, ISA, 10,000 ft; alternate 100 nm

Market potential

Description

Baseline ISR

1.Higher growth

2.Lower growth rate

3.Competition

4.Downside scenario

Baseline Commuter

2.1 Shrinking market

2.2 Competition


Generic market

997

1108

790

997

790

500

275

500

Dornier 228NG Share

19.8% = 197

19.8% = 219

19.8% = 156

16.6% = 166

16.6% = 131

21% = 105

21% = 58

18% = 92

Probability

High

Medium

Medium

Medium

Low

High

Low

Medium

Mean Time Between In-Flight Shutdown

(MTBIFSD)


Dornier 228 New Generation Honeywell TPE331 – Reliability

MT

BIF

SD

rate

per

1,0

00 h

our

0.0200

0.0150

0.0100

0.0050

0.0000

Jan-0

9

Feb-0

9

Mar-

09

Apr-

09

May-

09

Jun-0

9

Jul-09

Aug-0

9

Sep-0

9

Oct-

09

Nov-0

9

Dec-0

9

Jan-1

0

Feb-1

0

Mar-

10

Apr-

10

May-

10

Jun-1

0

Jul-10

Aug-1

0

Sep-1

0

Oct-

10

Nov-1

0

Dec-1

0

Goal = .01 events per 1.000 fleet hours (ie. 100.000 hours MTBIFSD)

MTBIFSD rate = 0.0 (> 658.578 hours) MT

BIF

SD

rate

per

1,0

00 h

our

0.0200

0.0150

0.0100

0.0050

0.0000

Jan-0

9

Feb-0

9

Mar-

09

Apr-

09

May-

09

Jun-0

9

Jul-09

Aug-0

9

Sep-0

9

Oct-

09

Nov-0

9

Dec-0

9

Jan-1

0

Feb-1

0

Mar-

10

Apr-

10

May-

10

Jun-1

0

Jul-10

Aug-1

0

Sep-1

0

Oct-

10

Nov-1

0

Dec-1

0

Goal = .01 events per 1.000 fleet hours (ie. 100.000 hours MTBIFSD)

MTBF rate = 0.14 (> 73.175 hours)

Mean Time Between Failure

(MTBF)

www.ruag.com

P.O. BOX 1253

82231 Wessling

Germany

© RUAG Aerospace Services GmbH 2012

ALL RIGHTS RESERVED

This document and all information contained herein is the sole property of RUAG Aerospace Services GmbH.

No intellectual property rights are granted by the delivery of this document or disclosure of its content.

This document shall not be reproduced or disclosed to a third party without the express prior written consent

of RUAG Aerospace Services GmbH.

This document and its content shall not be used for any other purpose other than for which it is supplied.

The statements made herein do not constitute an offer. They are based on the assumptions shown and are expressed in good faith.

Where the supporting grounds for these statements are not shown,

RUAG Aerospace Services GmbH will be pleased to explain the basis thereof.

Printed in Germany

A flexible and versatile special mission surveillance …tangentlink.com/wp-content/uploads/2013/09/2.-Meeting...5 RUAG Aviation 12.09.2013 Dornier 228 New Generation State-of-the-art

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