Ken Moritz and Bo GoodeNAVAIR PMA-27518 January 2004

V-22International

NAVY-INDUSTRY INTERNATIONAL DIALOG

Slide 2

The V-22and the

War onTerrorism

The V-22and the

War onTerrorism

Slide 3

Forces - Afghanistan [Prevent](without V-22)

KC-135

C-17 (2)

KC-135KC-135

KC-135

KC-135

C-5 (3)

C-5 (3)

KC-135 KC-135

KC-135

KC-135

2/75th

Rangers(100)

DOE Tech(10)

5th SFG(12)

AC-130 (3)

Physical security risk: = high= moderate= low

OPSEC considerations: = moderate profile = high profile

• 3 C-5s, helicopter teardown at Taegu

• 19 aircraft through Kadena

B-1 (3) MH-53M (4)

MH-47E (4)

MC-130H (3)

MC-130E (5)

Complex; Multiple Failure NodesComplex; Multiple Failure Nodes

Slide 4

KC-135

2/75th Rangers

(100)

DOETech (10)

5th SFG(12)

CV-22 (7)

Physical security risk: = high= moderate= low

OPSEC considerations: = moderate profile = high profile

Forces - Afghanistan [Prevent](with V-22)

KC-135

KC-135

C-17 (2) B-1 (3)

AC-130 (3)

KC-135

KC-135

MC-130H (3)

Simpler and More Likely to SucceedSimpler and More Likely to Succeed

Scenario Prevent 1 Support Costs Afghanistan

$388,035 $388,035 $2,307,342 $1,852,165

$6,846,330 $2,171,621 $610,801

+ + = $ 3,083,412

+ = $9,017,951

Total Air Costs $2,800,901$13,167,494

$566,131$337,935

(Not actual number of tankers) (Not actual number of tankers)

V-22 Multi-Mission Applications for the UK

Final ReportSeptember, 1999

THE TILTROTOR TEAM

Tilt-rotor Characteristics RequiredAdditional Missions

The basic V-22 airframe, with the appropriate mission kits or system modifications, is suitable for all of the eight additional missions which were examined, but not modelled.

The basic V-22 airframe, with the appropriate mission kits or system modifications, is suitable for all of the eight additional missions which were examined, but not modelled.

AttributeAirborne

Early Warning

Electronic Warfare

Command and Control

Air-to-Air Refueler

Logistic Support

Strategic Self-

Deployment

Combat Search and

Rescue

Special Operations

V/STOL (sea and land basing) 2 2 1 2 2 1 2 2

Fast climb/descent 2 2 1 1 1 1 2 2

Fast cruise 2 2 2 2 2 2 2 2

Fixed wing loiter 2 2 2 1 0 0 2 2

Mid-mission hover 1 1 2 1 2 0 2 2

Long range/endurance 2 2 2 2 2 2 2 2

In-flight refuel 1 1 1 2 1 2 2 2

Internal volume/payload 2 2 2 2 2 2 2 2

External lift/payload 0 0 0 0 2 0 1 1

Mission System Requirements

None (standard design airframe) X

Modular mission kit X X X X

Dedicated installation X X X X X

Enhanced DAS 1 1 1 0 0 0 2 2

Importance to Mission (2 = Essential, 1 = Desireable, 0 = Not Relevant)

THE TILTROTOR TEAM

Slide 9

Multi Mission Capability

• ASW– Large area search

– Small area localization

• Airborne mine countermeasures

• AEW

• Search and Rescue – Peacetime and combat

– 805 nm range (MV/HV mission)

• Command & Control

• NATO Reaction Force

• In Flight Refueling (tanker)

– At 600 nm radius, give away 2,500 lbs

– At 200 nm radius, give away 16,500 lbs

• COD/VOD/VERTREP

– 24 personnel

– 15,000 lbs cargo

– 20,000 lbs internal

• Special Operations

– Single aircraft ops

– Choice of USMC and SOCOM

Slide 10Public Web Site: http://pma275.navair.navy.mil

Slide 11

Slide 12

Take-Away

• Breaking the paradigm “It’s not a typical Helicopter, it’s a Tiltrotor”

– Flight characteristics better than a conventional Helo

– Significant increase in response time, survivability & maintainability

– Unit cost slightly higher than conventional Helo but yields returns in

capabilities + support footprint + manpower = lower operational cost

• Reduce Type Model Series and gain

– Multi-mission platform optimizes V-22 saving over life cycle

– Mission support structure optimized (manpower, facilities & other platforms)

– Interoperability with NATO and coalition partners

– Cooperative development program opportunities

– Support structure commonality