Attachment_0002_DVHA1_Performance_Spec.pdf

StrykerDVH-A1 FoV Performance

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

System Performance Specifications

For the

STRYKER Double “V” Hull (DVH-A1) Family of

Vehicles (FoV)

2017.11 Through 2017.20

W56HZV14CB019

Date: 12 December 2017

WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.) or the Export Administration Act of 1979 (Title 50, U.S.C., App. 2401 et seq.), as amended.

Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD

Directive 5230.25.

Date: 12 December 2017

2017.11: INFANTRY CARRIER VEHICLE (ICVV-A1) PERFORMANCE SPECIFICATION

1 INTRODUCTION

1.1 System Description

1.2 Scope

1.3 Key Performance Parameters (KPPs)

1.3.1 All Vehicles

1.3.2 ICVV

2 APPLICABLE DOCUMENTS

2.1 Order of Precedence

3 ICVV SYSTEM

3.1.1 Minimum Commonality Baseline

3.1.2 Mission Equipment Package

3.1 Infantry Carrier Vehicle (ICVV)

3.1.1 Vehicle System Requirements

3.1.1.1 Transportability

3.1.1.1.1 Air Transportability

3.1.1.1.2 Weight

3.1.1.1.2.1 Vehicle Production Weights

3.1.1.1.2.2 Full Combat Weight (FCW)

3.1.1.1.2.3 Gross Vehicle Weight Rating (GVWR)

3.1.1.1.2.4 General Test Conditions

3.1.1.1.3 Other Transportation

3.1.1.1.4 External Tie Downs

3.1.1.2 Personnel

3.1.1.2.1 Crew

3.1.1.2.2 Infantry Squad

3.1.1.2.2.1 Squad Equipment

3.1.1.3 Survivability

3.1.1.3.1 Reserved

3.1.1.3.2 Soldier Survivability

3.1.1.3.3 Penetration Avoidance

3.1.1.3.3.1 Mine and IED Protection

3.1.1.3.3.1.1 Other Mine Protection

3.1.1.3.3.2 Artillery Protection

3.1.1.3.3.3 Small Arms and Machine Gun Protection

3.1.1.3.3.4 Spall

3.1.1.3.3.5 Driver's Enhancement Kit (DEK) Accommodation

3.1.1.3.3.6 Hand Held Infantry Weapon Protection

3.1.1.3.3.7 SLAT Armor Accommodation

3.1.1.3.4 Reserved

3.1.1.3.5 Reserved

3.1.1.3.6 Obscuration

3.1.1.3.7 Rapid Ingress/Egress

3.1.1.3.8 Fire Detection and Suppression

3.1.1.3.8.1 Occupied Compartments

Date: 12 December 2017

3.1.1.3.8.1.1 Portable Fire Extinguisher Bottles

3.1.1.3.8.2 Unoccupied Compartments

3.1.1.3.8.3 Fire Detection and Suppression

3.1.1.3.8.4 Manual Activation

3.1.1.3.9 Laser Eye Protection

3.1.1.4 Environments

3.1.1.4.1 Natural Environment

3.1.1.4.1.1 Temperature

3.1.1.4.1.1.1 Operating

3.1.1.4.1.1.2 Non-Operating

3.1.1.4.1.2 Humidity

3.1.1.4.1.3 Fungus

3.1.1.4.1.4 Altitude

3.1.1.4.1.5 Solar Radiation

3.1.1.4.1.6 Sand

3.1.1.4.1.7 Dust

3.1.1.4.1.8 Rain

3.1.1.4.1.9 Snow

3.1.1.4.1.10 Salt Fog

3.1.1.4.1.11 Icing

3.1.1.4.1.12 Lightning

3.1.1.4.2 Induced Environments

3.1.1.4.2.1 Vibration

3.1.1.4.2.2 Shock

3.1.1.4.2.2.1 Reserved

3.1.1.4.2.2.2 Weapons Firing

3.1.1.4.2.3 Electromagnetic Environmental Effects (E3) Spectrum Supportability

3.1.1.4.2.3.1 Electrostatic Discharge (ESD)

3.1.1.4.2.3.2 Reserved

3.1.1.4.2.3.3 Electromagnetic Interference/Compatibility (EMI/EMC)

3.1.1.4.2.4 Nuclear, Biological, and Chemical (NBC)

3.1.1.4.2.4.1 NBC Detection

3.1.1.4.2.4.2 NBC Survivability

3.1.1.4.2.4.3 NBC Decontaminability

3.1.1.4.2.5 Reserved

3.1.1.4.2.6 High-Altitude Electromagnetic Pulse (HEMP)

3.1.1.5 Mobility

3.1.1.5.1 Hard Surface Roads

3.1.1.5.1.1 Reserved

3.1.1.5.1.2 Reserved

3.1.1.5.1.3 Reserved

3.1.1.5.1.4 Emergency Lane Change

3.1.1.5.2 Terrain

3.1.1.5.2.1 Vehicle Cone Index (VCI)

3.1.1.5.2.2 Full Power Testing (extrapolated temperatures)

3.1.1.5.2.3 Tractive Effort Testing

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.5.3 Vertical Climb

3.1.1.5.4 Minimum Cruising Range

3.1.1.5.5 Fording

3.1.1.5.6 Slope Performance

3.1.1.5.6.1 Engine Start on Slopes

3.1.1.5.7 Gap

3.1.1.5.8 Reserved

3.1.1.5.9 Ride Quality

3.1.1.5.9.1 Absorbed Power

3.1.1.5.9.2 Half Rounds

3.1.1.5.10 Braking

3.1.1.5.10.1 Service Brakes

3.1.1.5.10.2 Parking Brake

3.1.1.5.10.3 Emergency Brakes

3.1.1.5.10.4 Laurel Mountain Braking

3.1.1.5.11 Turning Radius

3.1.1.6 Sustainability

3.1.1.6.1 Towing

3.1.1.6.2 Self-Recovery

3.1.1.6.3 NATO Slave Receptacle

3.1.1.6.4 Fuel System

3.1.1.6.4.1 Fuel Shutoff

3.1.1.6.4.2 Fuel Scavenging

3.1.1.6.4.3 Fuel Leveling

3.1.1.6.5 Tire Inflation

3.1.1.6.6 Fuel and Lubrication

3.1.1.7 Logistics and Readiness

3.1.1.7.1 Maintenance

3.1.1.7.1.1 BIT/BITE and Embedded Diagnostics

3.1.1.7.1.2 Interactive Electronic Technical Manuals

3.1.1.7.1.3 LRU Replacement

3.1.1.7.1.4 Power Train Components

3.1.1.7.1.4.1 Engine Air Filtration

3.1.1.7.1.5 Unified Software Loader (USL) Support Requirement

3.1.1.7.2 Reliability

3.1.1.7.3 Maintainability

3.1.1.7.3.1 Daily Operator/Crew Checks

3.1.1.7.3.2 Standard Tools

3.1.1.7.3.3 Part Marking

3.1.1.8 Auxiliary Systems

3.1.1.8.1 Water Heater

3.1.1.8.2 Reserved

3.1.1.9 Painting and Other Metal Surface Finishes

3.1.1.9.1 Metal Surface Pretreatment

3.1.1.9.1.1 Aluminum

3.1.1.9.1.1.1 Conversion Coating…………………………………………………………………………...27

3.1.1.9.1.1.2 Anodizing……………………………………………………………………………………..27

3.1.1.9.1.2 Steel

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.9.2 Paint

3.1.1.9.3 Plating

3.1.1.10 MANPRINT

3.1.1.10.1 Reserved

3.1.1.10.2 Human Factors Engineering

3.1.1.10.3 Safety and Health Hazards

3.1.1.10.3.1 Exterior Lighting

3.1.1.10.3.2 Interior Lighting

3.1.1.10.3.3 Noise

3.1.1.10.4 Crew Hatch and Door Combat Locks

3.1.1.10.5 Hazard and Environmental Damaging Materials

3.1.1.10.6 Hatch Grab Handle and/or Grab Strap

3.1.1.10.7 Crew and Squad Seats

3.1.1.10.7.1 Drivers Extraction

3.1.1.10.7.2 Shock Attenuation

3.1.1.10.7.3 Crew Seats and Restraint System

3.1.1.10.7.4 Gunner’s Restraint

3.1.1.10.8 Driver’s Station Survivability

3.1.1.10.8.1 Steering Wheel

3.1.1.11 Electrical Power System

3.1.1.11.1.1 Electrical Power Generation

3.1.1.11.1.2 Power Storage

3.1.1.11.1.3 Electric Power Distribution

3.1.1.11.1.4 Silent Watch

3.1.1.12 Driver’s Vision

3.1.1.13 Periscopes

3.1.1.13.1 Driver’s Vision Periscopes

3.1.1.13.2 Commander’s Vision Periscopes

3.1.2 Subsystem Requirements

3.1.2.1 Command, Control, Communications, Computers, Intelligence, Surveillance and

Reconnaissance (C4ISR) Subsystem

3.1.2.1.1 External

3.1.2.1.1.1 General System Interoperability

3.1.2.1.1.2 Reserved

3.1.2.1.1.3 Reserved

3.1.2.1.1.4 Dismounted Soldiers

3.1.2.1.1.5 Co-site Interference

3.1.2.1.2 Internal

3.1.2.1.2.1 In-Vehicle Network (IVN)

3.1.2.1.2.1.1 Processing

3.1.2.1.2.1.2 Network Services

3.1.2.1.2.1.3 Multi Function Vehicle Port (MFVP)

3.1.2.1.2.2 Intercom

3.1.2.1.2.2.1 Full Function Crew Station (FFCS)

3.1.2.1.2.3 Displays

StrykerDVH-A1 FoV Performance Specifications

No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.2.1.2.3.1 Squad Leader’s Display

3.1.2.1.2.3.2 Commander’s Display

3.1.2.1.2.3.2.1 PM JBCP BFT2

3.1.2.1.2.3.3 Driver’s Display

3.1.2.1.2.3.4 Rear View Sensor System (RVSS)

3.1.2.1.2.3.5 Networked Displays

3.1.2.2 Weapons and Fire Control Subsystems

3.1.2.2.1 Remote Weapon Station System

3.1.2.2.1.1 STORM Secure Storage

3.1.2.2.2 Primary Armament

3.1.2.2.3 Secondary Armament

3.1.2.2.4 Target Acquisition

3.1.2.2.5 Storage

3.1.2.2.5.1 NATO Litter

3.1.2.2.6 Storm Lock Box

3.1.2.3 Climate Control System

3.1.3 Auxiliary Systems

3.1.3.1 Air Horn

3.2 Training Devices

3.3 Embedded Training System Software (ETSS)

3.3.1 Reserved

3.4 Reserved

3.5 Reserved

3.6 Kits

2017.12: MORTAR CARRIER VEHICLE (MCVV-A1) DELTA SYSTEM PERFORMANCE

SPECIFICATION

1.1 Introduction

1.2 System Description

1.3 Scope

1.3.2 ICVV

3.0.2 Mission Equipment Package

3.0.2.1 120mm Mortar System

3.0.2.1.1.1 Accelerated Precision Mortar Initiative (APMI)

3.0.2.1.1 Capability

3.0.2.1.2 Inspection Criteria

3.1.2.2 GFM Mortar Fire Control System (MFCS)

3.1.2.3 Integration

3.0.2.3.1 Emplacement/Displacement

3.1.2.3.2 Traverse/Elevation Capability

3.0.2.3.2.1 Travel Lock

3.1.2.3.3 Rate of Fire

3.1.2.3.4 Firing Range

3.1.2.3.5 Unintentional Firing

3.1.1.2.1 Crew

3.1.1.2.2 MC Squad

3.1.1.2.2.1 Squad Equipment

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.3.6 Obscuration

3.1.1.3.7 Rapid Ingress/Egress

3.1.1.4.2.2.2 Weapons Firing

3.1.1.7.2.1 Mortar System Reliability

3.1.1.7.2.2 Mortar System Durability

3.1.1.7.2.3 Mortar Fire Control System (MFCS) or equivalent Reliability

3.1.1.10.7.2 Shock Attenuation

3.1.2.1.2.2.1 Full Function Crew Station (FFCS)

3.1.2.2.1 Remote Weapon Station System

3.1.2.2.2 Primary Armament

3.1.2.2.3 Secondary Armament

3.1.2.2.5.1 Mortar and Ammunition Storage

2017.13: ANTI-TANK GUIDED MISSILE VEHICLE (ATVV-A1) DELTA SYSTEM PERFORMANCE

SPECIFICATION

1.1 INTRODUCTION

1.2 System Description

1.3.2 N/A

3.0.2 Mission Equipment Package

3.0.2.1 Target Acquisition / Fire Control

3.1 Anti-Tank Guided Missile Vehicle (ATVV)

3.1.1.2.1 Crew

3.1.1.2.2 Infantry Squad

3.1.1.2.2.1 Squad Equipment

3.1.1.4.2.2.2 Weapons Firing

3.1.1.7.2 Reliability

3.1.2.1.2.2.1 Full Function Crew Station

3.1.2.1.2.3.1 Squad Leader’s Display

3.1.2.1.2.3.2 Commander’s Display

3.1.2.2.1 Remote Weapon Station System

3.1.2.2.2 Primary Armament

3.1.2.2.2.1 Safe Launch Horizon………………………………………………………………………….42

3.1.2.2.3 Secondary Armament

3.1.2.2.5 Storage

3.1.2.2.6 Weapon Reloading

3.2.1.1 Embedded Training

2017.14: RECONNAISSANCE VEHICLE (RVV-A1) DELTA SYSTEM PERFORMANCE SPECIFICATION

2017.15: FIRE SUPPORT VEHICLE (FSVV-A1) DELTA SYSTEM PERFORMANCE SPECIFICATION

1.1 INTRODUCTION

1.2 System Description

1.3.2 ICVV

3.1.2 Mission Equipment Package

3.1.2.1 Target Acquisition

3.1.2.2 Cupola

3.1.2.3 Davit

3.1.2.4 Storage

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1 FSVV Vehicle

3.1.1.2.2 FSVV Squad

3.1.1.2.2.1 Squad Equipment

3.1.1.2.3 FSVV Fire Support Station

3.1.1.4.2.2.2 Weapons Firing

3.1.2.1.2.2.1 Full Function Crew Station (FFCS)

3.1.2.1.2.3.1.2 FS3 MEP

3.1.2.2.1 Remote Weapon Station System

3.1.2.2.2 Primary Armament

2017.16: ENGINEER SQUAD VEHICLE (ESVV-A1) DELTA SYSTEM PERFORMANCE

SPECIFICATION

1.1 INTRODUCTION

1.2 System Description

3.0.2 Mission Equipment Packages

3.0.2.1 Obstacle Neutralization Systems

3.0.2.1.1 Surface Mine Plow (SMP)

3.0.2.1.1.1 Installation

3.1.2.1.1.1.1 SMP Installation

3.1.2.1.1.1.2 Jettison Fitting Kit (JFK)

3.0.2.1.1.2 SMP Removal

3.0.2.1.1.3 Survivability

3.1.2.1.1.2 Mine Clearance

3.1.2.1.1.3 Power Requirements

3.1.2.1.1.1.5.1 Electrical Power Requirements

3.1.2.1.1.1.5.2 Hydraulic Requirements

3.0.2.1.1.1.6 Transportation

3.0.2.1.2 Mine Roller (MR)

3.0.2.1.2.1 Installation

3.1.2.1.2.1.1 JFK

3.1.2.1.2.1.2 MR Installation

3.0.2.1.2.2 MR Removal

3.0.2.1.2.3 Survivability

3.1.2.1.2.2 MR Maximum Ground Pressure

3.1.2.1.2.3 Power Requirements

3.1.2.1.2.3.1 Electrical Power Requirements

3.1.2.1.2.3.2 Hydraulic Requirements

3.0.2.1.2.6 Transportation

3.0.2.1.3 Magnetic Signature Duplicator (MSD) System

3.0.2.1.3.1 Installation

3.0.2.1.3.1.1 MSD Installation

3.0.2.1.3.1.2 MSD Removal

3.1.2.1.3.4 Magnetic Signature Projection

3.1.2.1.3.5 Electrical Power Requirements

3.1.2.1.4 Lane Marking System (LMS)

3.0.2.1.4.1 Installation

3.0.2.1.4.2 Removal

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.0.2.1.4.3 Survivability

3.1.2.1.4.4 Marker Deployment

3.1.2.1.4.5 Power Requirements

3.1.2.1.4.5.1 Electrical Power Requirements

3.1.2.1.4.5.2 Pneumatic Requirements

3.0.2.1.5 Angle Mine Plow (AMP)

3.0.2.1.5.1 Installation

3.1.2.1.5.1.1 JFK

3.1.2.1.5.1.2 AMP Installation

3.0.2.1.5.2 AMP Removal

3.0.2.1.5.3 Survivability

3.1.2.1.5.4 Mine Clearance

3.1.2.1.5.5 Power Requirements

3.1.2.1.5.5.1 Electrical Power Requirements

3.1.2.1.5.5.2 Hydraulic Requirements

3.0.2.1.5.6 Transportation

3.0.2.1.6 Straight Obstacle Blade (SOB)

3.0.2.1.6.1 Installation

3.1.2.1.6.1.1 JFK Installation

3.1.2.1.6.1.2 SOB Installation

3.0.2.1.6.2 SOB Removal

3.1.2.1.6.4 Obstacle Removal

3.1.2.1.6.5 Power Requirements

3.1.2.1.6.5.1 Electrical Power Requirements

3.1.2.1.6.5.2 Hydraulic Requirements

3.0.2.1.6.6 Transportation

3.1.1.6.1.1 Through Hull Connector

3.1.1.6.1.2 Trailer Power Connector

3.1.2.1.2.2.1 Full Function Crew Station (FFCS)

2017.17: COMMANDER’S VEHICLE (CVV-A1) DELTA SYSTEM PERFORMANCE SPECIFICATION

1.0 INTRODUCTION

1.1 System Description

1.3.2 ICVV

3.0.2 Mission Equipment Package

3.0.2.1 Communications

3.1 Commander’s Vehicle (CVV)

3.1.1.2.1 Crew

3.1.1.2.2 CVV Squad

3.1.1.10.7.2 Shock Attenuation

3.1.2.1.2.2 Intercom

3.1.2.1.2.4 Operator Stations

3.1.2.1.2.4.1 All Source Analysis System (ASAS)

3.1.2.1.2.4.2 Maneuver Control System (MCS)

3.1.2.1.2.2.1 Full Function Crew Station (FFCS)

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

2017.18: MEDICAL EVACUATION VEHICLE (MEVV-A1) D E L T A SYSTEM PERFORMANCE

SPECIFICATION

1.0 Introduction

1.1 System Description

1.2 Scope

1.3.2 ICVV

2.0.1 MEVV Applicable Documents

3.1.2 MEVV

3.1.2.1 Mounting Capability

3.1.2.2 Interior Storage/Working Space

3.1.2.3 Litter Clearance

3.1.2.4 IV Bag Holders

3.1.2.5 Oxygen

3.1.2.6 Medical Communications

3.1.2.8 Markings

3.1.2.9 Litter Lift System

3.1.1.2.1 Crew

3.1.1.2.2 Infantry Squad

3.1.1.2.2.1 Squad Equipment

3.1.1.3.6 Obscuration

3.1.1.3.7 Rapid Ingress/Egress

3.1.1.4.2.2.2 Weapons Firing

3.1.1.10.3.2 Interior Lighting

3.1.2.1.2.2.1 Full Function Crew Station

3.1.2.1.2.3.1.1 Squad Leader’s Display

3.1.2.2 Weapons and Fire Control System

3.1.2.2.5.1 NATO Litter

: NUCLEAR, BIOLOGICAL, CHEMICAL RECONNAISSANCE VEHICLE (NBCRVV-A1) DELTA SYSTEM

PERFORMANCE SPECIFICATION

: MOBILE GUN SYSTEM (MGSV-A1) DELTA SYSTEM PERFORMANCE SPECIFICATION

4.0 VERIFICATION

4.1 Requirements Verification

4.1.1 Responsibility for inspection

4.1.2 Responsibility for compliance

4.1.3 Government verification

4.1.4 Production Verification Test (PVT)

4.1.5 First production vehicle inspection (FPVI)

4.1.5.1 In-process inspection

4.1.5.2 Completed vehicle inspections

4.1.5.2.1 Contractor inspection

4.1.5.2.2 Preliminary inspection

4.1.5.2.3 Test Failure……………………………………………………………………………………………58

4.1.5.2.4 FPVI Re-Inspection…………………………………………………………………………………

4.1.6 Quality conformance inspection (QCI)

4.1.6.1 QCI failure……………………………………………………………………………………………..58

4.2.0 Control test

4.2.1 Vehicle selection

4.2.2 Frequency

4.2.3 Test Failure

TABLE 5

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

CLASSIFICATION OF INSPECTION AND TESTS

List OF TABLES

Table 1: Applicable Documents

Table 2: V70 Speeds in MPH (Average Speed over 70% of the Terrain)

Table 3: CTIS Controller Settings

Table 4: USL Support Requirements

Table 5: Classification of Inspection and Tests

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

2017.11: Infantry Carrier Vehicle (ICVV-A1) Performance Specification

1 INTRODUCTION

1.1 System Description.

The Stryker Family of Vehicles (FoV) will provide the primary combat and combat support platform for the Stryker Brigade Combat Team (SBCT). The FoV will be employed as an integral part of the SBCT within a Divisional or Corps C4ISR structure. The Infantry Carrier Vehicle (ICVV) will be the baseline vehicle in the FoV.

1.2 Scope

The ICVV is comprised of the ICVV and its respective subsystems, and exterior interfaces.

1.3 Key Performance Parameters (KPPs)

1.3.1 All Vehicles

The following performance parameters apply to the FOV:

Interoperability (Paragraph 3.1.2.1.1.1)

1.3.2 ICVV

The following key performance parameter applies to the ICVV:

Infantry Squad (Paragraph 3.1.1.2.2)

2 Applicable Documents.

The following documents shall be applicable to the degree specified in the text and at the revision level published prior to June 1, 2000 or, as otherwise identified in the table below.

Table 1: Applicable Documents

Standards Title

Army Regulations

AR 70-38 Research, Development, Test and Evaluation of

Materiel for Extreme Climatic Conditions

C-130 certification [25 February 2011]

DoD Adopted Industry Standards

SAE J 336 Sound Level for Truck Cab Interior

ASTM F1941-10 Electrodeposited Coatings on Threaded Fasteners

(Unified Inch Screw Threads

ASTM B633-11 Electrodeposited Coatings of Zinc on Iron and

Steel

Federal Motor Vehicle Safety Standards

FMVSS 108 Lamps, Reflective Devices and Associated

Equipment

FMVSS 121 Air Brake System

FMVSS 207 Seating Systems

FMVSS 209 Seat Belt Anchoring

Federal Specification

A-A-52550 Pintle Assembly, Towing, Manual Release, 18000, 40000 and 100000 lbs Capacity

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

A-A-52557 Fuel, Oil, Diesel

KKK-A-1822 Star-Of-Life Ambulance

Military Handbooks

Failure Definition/Scoring Criteria Appendices A, B, D, E-F Update 3, Dated April

03, Appendix C dated 28 Feb 03

Interim Armored Vehicle (IAV) Operational Mode

Summary/Mission Profile (OMS/MP)

Version dated 2004

Stryker Nuclear, Biological and Chemical

Reconnaissance Vehicle Operational Mode

Summary/Mission Profile

Annex I, dated June 2007

(no standard #) Medical Evaluation of Non-Fragment Injury

Effects in Armored Vehicle Live Fire Test, Instrumentation Requirements and Injury Criteria

Dated September 1989

Military Specifications

MIL-A-8625 Rev F Anodic Coatings for Aluminum and Aluminum

Alloys

MIL-DTL-38999 Rev L & Mil-DTl-38999 Rev L

Supplement 1

Connectors, Electrical, Circular, Miniature, High

Density, Quick Disconnect (Bayonet, Threaded and

Breech Coupling), Environment Resistant, MIL-DTL-53039B Coating, Aliphatic Polyurethane, Single

Component, Chemical Agent Resistant

MIL-DTL-5541 Rev F Chemical Conversion Coating of Aluminum and

Aluminum Alloys

MIL-DTL-53072 Rev C Chemical Agent Resistant Coating (CARC) System

Application Procedures and Quality Control

Inspection

MIL-DTL-62420 Rev B (AT) Periscope, Tank

MIL-DTL-62422C(AT) Filter, Laser Hazard Protection

MIL-DTL-83133 Turbine Fuels, Aviation, Kerosene Types, NATO

F-34 (JP-8), and NATO F-35, and JP-8+100

MIL-PRF-22750 Coating, Epoxy, High Solids

MIL-PRF-39532 TOW 2B Performance Specification

MIL-STD-1275 Rev A Characteristics of 28 Volt DC Electrical Systems in

Military Vehicles

MIL-STD 130 Identification marking of U.S. Military Property

MIL-STD-1366 Interface Standard for Transportability Criteria

MIL-STD-1472 Rev F Human Engineering

MIL-STD-1474 Noise Limits

MIL-STD-1686C Electrostatic Discharge Control Program for

Protection of Electrical and Electronic Parts

Assemblies and Equipment (Excluding Electrically

Initiated Explosive Devices)

MIL-STDHDBK-1791 Designing for Internal Arial Delivery in Fixed

Wing Aircraft

MIL-STD-209 Rev J Interface Standard for Lifting and Tie down Provisions

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

MIL-HDBK-310 Climatic Information to Determine Design and Test

Requirements for Military Systems and Equipment

MIL-STD-461 Rev E Requirements for the Control of Electromagnetic

Interference Characteristics of Subsystems and

Equipment

MIL-STD-810E Environmental Test Methods and Engineering

Guidelines

MIL-STD-882 System Safety Program Requirements

MIL-T-704 Treatment and Painting of Materiel

JTA-A Department of the Army Joint Technical

Architecture-Army (JTA-A) Version 6.0 Dated 3

October 2003

Miscellaneous

U.S.C. § 7401 Clean Air Act of 1990

ARD-110 120mm Mortar System Specification

NATO Mobility Model NATO Reference Mobility Model (NRMM)

NRMM II Version 2.7.0

System Resource Flow Description (SV-2) and

Standards Profile (StdV-1) of the Information

Support Plan (ISP), and Government provided

Vehicle Configuration Diagrams

Dated 5 February 2008

MIL- DTL-83133 Rev E JP8

2.1 Order of Precedence

In the event of a conflict between the text of this specification and the references cited, the text of this specification shall take precedence. Nothing in this specification, however, supersedes applicable laws and regulations unless there is a specific exemption.

3 ICVV System

3.1.1 Minimum Commonality Baseline

The ICVV shall maintain maximum commonality at the system, subsystem, essential Line Replaceable

Unit (LRU), and maintenance significant spare and repair level with other variants / configurations of the

FoV. LRUs are defined as essential items or assemblies that can be removed from the vehicle and replaced

(at the field level) as a single unit to restore the vehicle to an operationally ready condition. Maintenance significant spare and repair parts are defined as those items removed and replaced and identified by

National Stock Number (NSN) in a Repair Parts & Special Tools List or offered Contractor Logistics

Support (CLS) parts catalog. For the purpose of this acquisition field level maintenance is defined as maintenance performed within the brigade by personnel assigned to the brigade support battalion or as a crew member of the FOV. Commonality shall be maximized within the Stryker FoV for platform mission functionality, operator and crew positions and tasks, maintenance tasks and required skills, required tools and TMDE, to result in expedience and reduced training and logistics burdens within the BCT, within the division (limited conversion Force XXI Division and Light Infantry Division), and within DoD.

3.1.2 Mission Equipment Package

Reserved

3.1 Infantry Carrier Vehicle (ICVV)

The ICVV shall be capable of operating effectively, employ weapon systems, and rapidly maneuver during blackout, day / night operations, inclement weather, and in periods of limited visibility.

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1 Vehicle System Requirements

The mission critical components, integrated in the vehicle, shall operate effectively across the operating environments specified in Paragraph 3.1.1.4.

3.1.1.1 Transportability

3.1.1.1.1 Air Transportability.

The Stryker ICVV shall be capable of air transport in C-5 and C-17 aircraft IAW MIL-STD-1366 and

MIL-HDB-1791. The Stryker ECP vehicle shall be capable of non-operating “cabin” altitudes of up to

15,000 feet (8.3 psi) per MIL-STD-810E. The Stryker ECP vehicle shall be capable of transport on aircraft without any hazard to personnel, the aircraft or the vehicle when exposed to an internal pressure differential of 8.3 psi developed in 0.5 seconds or less due to rapid decompression. (Reference MIL-

HDBK-1791, paragraph 5.2.5.2).

3.1.1.1.2 Weight

3.1.1.1.2.1 Vehicle Production Weights

The ICVV, with all equipment to include Government Furnished Material (GFM), shall not exceed the following weight:

ICVV 52,000 lbs. (TBR)

CVV 52,500 lbs. (TBR)

FSVV 52,500 lbs. (TBR)

ESVV 53,000 lbs. (TBR)

ATVV 54,000 lbs. (TBR)

MCVV 55,000 lbs. (TBR)

MEVV 54,000 lbs. (TBR).

3.1.1.1.2.2 Full Combat Weight (FCW)

The FCW of the ICVV shall be the vehicle production weight plus BII, COEI, AAL, and ASIOE mission equipment including fuel and ammo and personnel added to the vehicle production weight not to exceed the following:

ICVV 57,500 lbs. (TBR)

CVV 56,000 lbs. (TBR)

FSVV 55,500 lbs. (TBR)

ESVV 59,000 lbs. (TBR)

ATVV 57,000 lbs. (TBR)

MCVV 60,000 lbs. (TBR)

MEVV 56,500 lbs. (TBR).

3.1.1.1.2.3 Gross Vehicle Weight Rating (GVWR)

The Stryker ICVV shall have a GVWR of 63,000 lbs.

3.1.1.1.2.4 General Test Conditions

Unless otherwise stated, the general test conditions for the Stryker ICVV vehicle are:

a. 550 amp power draw from alternator

b. Vehicle frontal area of 91.84 ft2

c. Drag coefficient of 1.2

d. Cooling fan speed representative of test condition

e. GVW of 60,000 lbs.

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.1.3 Other Transportation

The ICVV shall be capable of transport using existing land, rail, and ship capabilities. Tie-down and lifting provisions shall be in accordance with MIL-STD-209 with the exception of 5.1.2b. The minimum sling length required to meet the requirements of MIL-STD-209 5.1.2b shall be no less than

17.5 feet. The Stryker shall not deform or degrade when tested IAW MIL-STD-810E Method 516

Procedure VIII Rail Impact Shock.

3.1.1.1.4 External Tie Downs

The ICVV shall be equipped with outside cargo straps and hooks.

3.1.1.2 Personnel

Squad does not include crew unless otherwise noted.

3.1.1.2.1 Crew

The combat loaded ICVV shall be fully operable by and accommodate (for 72 hours) a crew of at least

2 with individual equipment including 2 sets of Chemical Biological Radiological Nuclear CBRN protective clothing and food per crew member and two (2) five (5) gallon water cans. The crew shall be designated as the driver and commander.

3.1.1.2.2 Infantry Squad

The combat loaded ICVV shall be capable of carrying an infantry squad (9 soldiers with individual equipment), equipped for any season clothing (cold weather).

3.1.1.2.2.1 Squad Equipment

The ICVV shall have a load plan for crew and squad equipment. The ICVV shall provide space for each squad member, food/ water for 72 hours and two (2) sets per squad member of NBC protective clothing.

3.1.1.3 Survivability

Reference Classified Appendix 4.

3.1.1.3.1 Reserved

3.1.1.3.2 Soldier Survivability

The ICVV shall minimize the potential for fratricide, minimize detectability and minimize damage if attacked.

3.1.1.3.3 Penetration Avoidance

3.1.1.3.3.1 Mine and IED Protection

The ICVV shall protect the crew and squad against the blast, acceleration and overpressure effects of mines and IEDs detonated anywhere under the vehicle. The protection levels shall be in accordance with (IAW) the DVH Delta Classified SPS.

3.1.1.3.3.1.1 Other Mine Protection

The ICVV shall include ballistic mine protection in the form of ballistic floor plates, Height

Management System (HMS) and Mine Protection Kits. Mine Protection Kits shall provide increased protection to the crew from an underbelly blast threat. The HMS shall provide a setting for vehicle height at 35 mm ± 5 mm above nominal.

3.1.1.3.3.2 Artillery Protection

The ICVV shall provide overhead, all around protection for the squad and crew from Classified

Artillery high explosive airburst or point detonation at Classified meters from the vehicle (all around), and at Classified meters directly above the vehicle (overhead). Level of overhead and all around protection coverage shall be as detailed in the Classified Appendix 4.

3.1.1.3.3.3 Small Arms and Machine Gun Protection

The ICVV shall provide integral protection to the crew, squad and engine compartment against small arms. The specific threats, levels of protection coverage and threat ranges shall be as defined in the

Classified Appendix 4.

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.3.3.4 Spall

The crew compartment shall minimize the effects of spall (i.e. spall liner or equivalent).

3.1.1.3.3.5 Driver's Enhancement Kit (DEK) Accommodation

Not Applicable

3.1.1.3.3.6 Hand Held Infantry Weapon Protection

The ICVV shall be provided with the capability to mount add on scalable armor packages (active or passive) to protect against hand held infantry weapon (Reference Classified Appendix 4). Packages must include full frontal, side and rear protection. During the process of protecting the vehicle, the scalable armor shall not endanger personnel and equipment in close proximity to the vehicle.

Minimum safe zone shall be classified meters from the vehicle. Packages shall have minimal impact on deployability and mobility profiles. Packages shall be soldier mountable/dismountable within 6 hours

(required) with no special tools requirements. Specific RPGs to be protected against are defined in the

Classified Appendix 4)

3.1.1.3.3.7 SLAT Armor Accommodation

The ICVV shall have mounting provisions for Stryker SLAT Armor.

3.1.1.3.4 Reserved

3.1.1.3.5 Reserved

3.1.1.3.6 Obscuration

The ICVV shall be capable of detection avoidance by rapid multi-spectral self-obscuration activated manually from inside the vehicle by the vehicle commander and/or driver. The system shall provide

360 degree visual/infrared/millimeter wave detection avoidance screening protection.

3.1.1.3.7 Rapid Ingress/Egress

The ICVV crew doors and hatches shall permit rapid ingress/egress of 5th through 95th percentile crewman while in full combat gear. Egress through the crew’s primary roof hatches shall not exceed

30 seconds. Egress through the crew’s secondary pathway shall not exceed one minute.

3.1.1.3.8 Fire Detection and Suppression

The ICVV shall have a fire detection and suppression system. The system shall be integrated with a prime power interrupter that interrupts battery power to the vehicle electrical system when master power is shut off. The system shall not contain Class I or Class II ozone depleting chemicals as specified in 52.223-4002

3.1.1.3.8.1 Occupied Compartments

The fire extinguishing system in the occupied compartments shall utilize FM200 with 5% - 10% sodium bicarbonate and be capable of extinguishing peacetime and combat initiated Petroleum, Oil, and Lubricant (POL) fires before crewmen receive second degree burns. Compartment overpressures, agent concentrations, by-products, and oxygen levels shall be acceptable to U.S. Army Surgeon

General (ref: Medical Evaluation of Non-Fragment Injury Effects in Armored Vehicle Live Fire Test, Instrumentation Requirements and Injury Criteria Dated September 1989). The system shall be automatic with manual backup capability.

3.1.1.3.8.1.1 Portable Fire Extinguisher Bottles

The vehicle shall stow two (2) portable sodium bicarbonate fire extinguisher bottles readily accessible to the Commander and Driver respectively.

3.1.1.3.8.2 Unoccupied Compartments

The vehicle shall have an automatic fire detection and extinguishing system with a manually activated backup capability in the unoccupied compartments that extinguishes POL fires within 10 seconds of detection. The system shall function either with the engine running or not running.

3.1.1.3.8.3 Fire Detection and Suppression

The fire detection and suppression system shall include an uninterrupted power source capable of maintaining system functionality for a period of 30 minutes after vehicle shutdown or loss of power as a threshold requirement.

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.3.8.4 Manual Activation

The ICVV shall include manual activation of the fire suppression system from the crew compartment to include functionality similar to the controls in the driver’s station.

3.1.1.3.9 Laser Eye Protection

ICVV unity vision devices shall incorporate a laser hazard protection filter using MIL-DTL-

62422C(AT) as a guide. The ICVV shall provide eye protection from battlefield lasers when viewing in a direct view sight. Filters shall provide eye protection against both friendly and hostile lasers and designators.

3.1.1.4 Environments

The ICVV shall meet or exceed specified safety and performance requirements during and after exposure to natural and induced environments as described below.

3.1.1.4.1 Natural Environment

3.1.1.4.1.1 Temperature

3.1.1.4.1.1.1 Operating

The ICVV shall be capable of operating in exterior ambient temperatures from -51° F/-46°C to

+125°F/+52°C. A kit may be used to operate below -25°F/-32°C exterior ambient. The ICVV shall provide a fuel fired heater capable of achieving and maintaining the interior operating temperature of

+39°F/+4°C within one hour after being cold soaked at -29°F/-34°C for at least 12 hours.

Temperatures within the vehicle shall not cause degradation to or failure of the electronic systems/subsystems. The commercial CFE/CFM computer/electronic components shall be capable of operating in temperatures from 0°F/-18°C to +120°F/+49°C.

3.1.1.4.1.1.2 Non-Operating

The ICVV shall not suffer performance degradations after being subjected to non-operating temperatures from -60°F/-51°C to +160°F/+71°C. The commercial CFE/CFM computer/electronic components shall be capable of operating after exposure to non-operating temperatures from -25°F/-32 degrees C to +149°F/+65 degrees C.

3.1.1.4.1.2 Humidity

The ICVV shall be capable of operating without performance degradation during and after exposure to hot-humid conditions as per MIL-STD-810E.

3.1.1.4.1.3 Fungus

The ICVV shall operate without damage or degradation from fungal effects as defined in MIL-STD-

810E when operating in hot humid climates as defined in MIL-HDBK-310.

3.1.1.4.1.4 Altitude

The ICVV systems, and sub-systems shall be capable of withstanding, without preparation or any degradation in performance, the altitude requirements of MIL-STD-810E. The ICVV shall be capable of operating without engine power degradation up to elevations of 5000 feet.

3.1.1.4.1.5 Solar Radiation

The ICVV shall be capable of operating without performance degradation during and after exposure to

1120 watts/m2 normal incident solar radiation at +120°F/+49°C.

3.1.1.4.1.6 Sand

The ICVV vehicle shall be capable of operating in heavy sand environments without performance degradation as defined in MIL-STD-810E. When conductance of mission is suspended due to poor visibility caused by blowing sand, the vehicle shall be suitably protected by applying the engine grill cover and vehicle tarpaulin supplied with the vehicle.

3.1.1.4.1.7 Dust

The ICVV shall operate without performance degradation during and after exposure to blowing dust for 6 hours.

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.4.1.8 Rain

The ICVV shall be capable of operating without degradation after exposure to heavy rainfall as defined in MIL-STD-810E. During heavy rainfall, the power package shall be capable of operating without damage or degradation. Since the grill openings in the engine compartment permit entry of rain through the air passages for cooling system, the vehicle shall provide a means for draining any water accumulated using drain plugs, and a grill cover shall also be supplied to minimize entry of rain or debris into the engine compartment when the vehicle is not operating.

3.1.1.4.1.9 Snow

The ICVV shall be capable of driving through 3 feet of dry, powder snow or 16 inches of heavy snow without preparation or tire chains.

3.1.1.4.1.10 Salt Fog

The ICVV shall operate without performance degradation during and after exposure to a salt fog concentration of 5±1 percent for 48 hours as per MIL-STD-810E, Method 509.3.

3.1.1.4.1.11 Icing

The ICVV shall operate during and after exposure to icing rain as per MIL-STD-810E, Method 521.1 for glazed ice up to 6mm thick.

3.1.1.4.1.12 Lightning

The ICVV and its subsystems shall remain operational after a near lightning strike as defined in MIL-

STD 464 Table IIB without adverse impact to the vehicle or crew.

3.1.1.4.2 Induced Environments

3.1.1.4.2.1 Vibration

The ICVV shall operate without performance degradation or damage from the effects of vibration during conductance of mission or transport IAW MIL-STD-810 Method 514.

3.1.1.4.2.2 Shock

The ICVV shall be capable of withstanding high levels of induced shock encountered during various modes of operation and transport including traversing difficult cross country terrain, and transport on fixed wing aircraft. The ICVV shall also be capable of withstanding without performance degradation, high impact loads resulting from rail hump testing, conducted in accordance with MIL-STD-810E.

3.1.1.4.2.2.1 Reserved

3.1.1.4.2.2.2 Weapons Firing

ICVV electronics and controls operation shall not be degraded after exposure to the RWS weapon firing induced loads.

3.1.1.4.2.3 Electromagnetic Environmental Effects (E3) Spectrum Supportability

All components of the ICVV shall be mutually compatible with other electronic equipment (CFE and

GFE) within the ICVV expected operational electromagnetic environment. All spectrum dependent equipment shall conform to the frequency spectrum certified for Army use worldwide, to include where the U.S. has a forward-based military presence. The vehicle shall comply with these requirements as tested with all hatches, doors, etc. closed.

3.1.1.4.2.3.1 Electrostatic Discharge (ESD)

All components that include sensitive electronics elements shall include appropriate enclosures, bonding and grounding to protect them from ESD from crew contact.

3.1.1.4.2.3.2 Reserved

3.1.1.4.2.3.3 Electromagnetic Interference/Compatibility (EMI/EMC)

No component, assembly, or subsystem performance shall be affected when other component, assembly, or subsystems are singularly or collectively operated IAW MIL-STD-461 and MIL-STD-

462D with all vehicle hatches, doors, etc. closed.

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.4.2.4 Nuclear, Biological, and Chemical (NBC)

3.1.1.4.2.4.1 NBC Detection

The ICVV shall use the Joint Chemical Agent Detector (JCAD) and Radiac to detect chemical agents and radiological fallout. The JCAD and Radiac shall have no degradation of performance after integration.

3.1.1.4.2.4.2 NBC Survivability

The ICVV shall be capable of performing critical functions while operating in a CBRN contaminated environment. The ICVV shall provide additional crew and squad protection through a ventilated face piece system.

3.1.1.4.2.4.3 NBC Decontaminability

The ICVV shall carry and store onboard one M100 and one M13 Decontamination Apparatus, Portable

(DAPs or M100 with equivalent size and weight) and one M295 Decontamination Kit, Individual

Equipment (DKIE) to conduct Immediate Decontamination within 15 minutes with no more than minimal damage to ICVV or installed equipment. The ICVV shall be decontaminable to avoid further transfer of contamination to operators, passengers, other equipment, and terrain following Operational

Decontamination. The ICVV shall be capable of decontamination to negligible risk levels following thorough decontamination procedures. If variants incorporate unique key components deemed necessary to be decontaminable to a negligible risk level, the identified component shall be decontaminable to a negligible risk level by the crew utilizing on-board decontamination equipment.

3.1.1.4.2.5 Reserved

3.1.1.4.2.6 High-Altitude Electromagnetic Pulse (HEMP)

The ICVV shall be capable of rebooting or restarting and returning to full operational capability within

15 minutes of a HEMP event. The ICVV shall not be required to operate through a High-altitude

Electromagnetic Pulse.

3.1.1.5 Mobility

3.1.1.5.1 Hard Surface Roads

The ICVV (under General Test Conditions per paragraph 3.1.1.1.2.4) shall be capable of sustained hard dry surface speeds of at least 60 mph at the appropriate highway Central Tire Inflation System

(CTIS) setting for the vehicle configuration. Hard dry surface is defined as a flat level paved surface free from moisture and debris. The CTIS setting is based on the maximum tire load as defined by the tire manufacturer. The Stryker ICVV (under General Test Conditions per paragraph 3.1.1.1.2.4) shall be capable of moving 50 meters from a standing start in less than 9 seconds on a hard dry surface measured from start of vehicle movement. The fuel shall be JP8. Brake stand starts are permissible.

3.1.1.5.1.1 Reserved

3.1.1.5.1.2 Reserved

3.1.1.5.1.3 Reserved

3.1.1.5.1.4 Emergency Lane Change

The ICVV shall be capable of safely negotiating an emergency lane change maneuver on the NATO course, NATO AVTP 03-160W (Ref 37, App C), at 42 mph on a level, paved asphalt road surface test course.

3.1.1.5.2 Terrain

The ICVV (under General Test Conditions per paragraph 3.1.1.1.2.4) shall be capable of operating over cross-country terrain. The mobility characteristics shall be quantified against target data below using North Atlantic Treaty Organization (NATO) Reference Mobility Model (NRMM) NRMM II

Version 2.7.0.

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

Table 2: V70 Speeds in MPH (Average Speed over 70% of the Terrain)

Germany

(LAUTREBACH)

Mideast

(MAFRAQ)

Korea Cheorwon)

Terrain Dry Wet Snow Dry Wet Sand Dry-Oct Wet-Oct

Tactical

Standard

15.8 8.9

(V50)

11.4

18.7 17.4 12.0 9.8 (V60)

8.0

Maximum

% No-Go

10.1 50.9 28.2

7.5 7.8

24.3 27.0 29.3

3.1.1.5.2.1 Vehicle Cone Index (VCI)

The ICVV at FCW shall have a single pass vehicle cone index (VCI) with cross country tire inflation pressure of no greater than 40.8. VCI (Vehicle Cone Index) can be defined as a minimum soil strength that is required in order for the vehicle to just maintain mobility. VCI-1 is for the vehicle to make one pass and VCI-50 is for the vehicle to make 50 passes. The vehicle with lower VCI is a better soft-soil performer.

3.1.1.5.2.2 Full Power Testing (extrapolated temperatures)

The ICVV shall operate at continuous full power to a maximum ambient temperature of 120 °F/49 °C

(hot-dry), per AR 70-38,with the climate control system off, without exceeding subsystem fluid operating temperature requirements. Subsystem fluids tested are: engine, transmission, transfer-case, hydraulics, and fuel delivery.

3.1.1.5.2.3 Tractive Effort Testing

The ICVV shall operate at a continuous tractive effort ratio of 0.62 (tractive effort in lbsf / vehicle test weight of 60,000 lbs) to a maximum ambient temperature of 120 °F/49 °C (hot-dry), per AR 70-38, with climate control system off, without exceeding subsystem fluid operating temperature requirements. Subsystem fluids tested are: engine, transmission, transfer-case, hydraulics, and fuel delivery.

3.1.1.5.3 Vertical Climb

The ICVV shall be capable of climbing vertical 23-inch obstacles in forward and reverse.

3.1.1.5.4 Minimum Cruising Range

The ICVV (under minimal automotive parasitic loads) shall be capable of a minimum cruising range of

300 miles at a speed of 40 mph on a hard dry level surface without refueling.

3.1.1.5.5 Fording

The ICVV shall be capable of fording (forward and reverse), while maintaining wheel contact with the ground, without preparation, water obstacles a minimum of 1.3 meters in depth. The vehicle shall also have a maximum static leakage rate into the crew compartment of less than 0.53 gallons/minute (2 l/m), when setting in approximately 1.3 meters of water. The vehicle shall also have a maximum spray leakage rate into the crew compartment of less than 2.0 gallons/minute (7.5 l/m) when all exposed hatches, doors, vision block, and periscopes are sprayed from a 5/8” hose with a water pressure of 55 psi for ten minutes from all exterior directions.

3.1.1.5.6 Slope Performance

The ICVV shall be capable of climbing and descending hard surface 60 percent frontal slopes and travel hard surface side slope of 30 percent, with no degradation in steering or creation of lack of lubrication or fluid leakage.

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.5.6.1 Engine Start on Slopes

The ICVV shall be capable of a main engine start on 60 percent frontal and 30 percent side slopes, after five minutes with engine off with 50 percent fuel on board.

3.1.1.5.7 Gap

The ICVV, at combat weight, shall be capable of crossing a gap perpendicular to the vehicle (1/4 vehicle length or 3 feet whichever is greater). Vehicle length is the distance from nose to rear ramp.

3.1.1.5.8 Reserved

3.1.1.5.9 Ride Quality

3.1.1.5.9.1 Absorbed Power

The ICVV shall attain no more than 6 watts average vertical absorbed power at the driver’s station seat pan, at the following speeds, on terrain at the stated inches RMS elevations at gross vehicle weight:

with the tires at normal cross country inflation pressure 45 mph at 0.7 in RMS, 35 mph at 1.0 in RMS, and 20 mph at 1.5 in RMS (Reference TOP 01-1-014A).

3.1.1.5.9.2 Half Rounds

The vehicle shall attain no more than 2.5g vertical peak acceleration at the driver's station seat pan at the following speeds over half round obstacles at the stated height at gross vehicle weight, with tires at normal cross country inflation pressure 40 mph at 8 in, 25 mph at 10 in (Reference TOP 01-1-014A).

3.1.1.5.10 Braking

The ICVV shall have a redundant system so that a single point failure does not cause a complete failure of the system. All brakes shall be self-adjusting. All brake linings/pads shall be constructed from non-asbestos materials. The vehicle shall be equipped with a brake on each axle end. All vehicles will incorporate anti-lock brakes and glad hands to support trailer air-brake systems.

3.1.1.5.10.1 Service Brakes

The ICVV braking system shall comply with the year 2000 version of FMVSS-121 at GVWR.

3.1.1.5.10.2 Parking Brake

The parking brake system shall be capable of holding the ICVV wheels from rotating when braking is applied, at GVWR, on a 60 percent grade, headed up or downgrade, on a dry hard surface free from loose material when the engine is off and the transmission in neutral. An indicator light shall alert the driver when the parking brake is engaged. The parking brake system shall be capable of being applied and released by the driver and be immediately available for re-applications. Braking energy shall not be dependent on maintenance of air or hydraulic pressure or electrical energy.

3.1.1.5.10.3 Emergency Brakes

The emergency brake system (i.e., the remaining half of the service brake system), in the event of a single point failure in the service brake system, shall stop the vehicle, at GVWR, at least once on a 30 percent slope and, shall remain engaged until intentionally disengaged by operating personnel.

Emergency braking system shall include a means of providing vehicle stopping in the event of a trailer breakaway.

3.1.1.5.10.4 Laurel Mountain Braking

The ICVV, at FCW, shall meet brake fade performance and safety characteristics by successfully completing the test procedures specified in the Laurel Mountain Brake Test Material Test Procedure

MTP 2-2-608.

3.1.1.5.11 Turning Radius

The ICVV (under General Test Conditions per paragraph 3.1.1.1.2.4) shall be capable of negotiating a

360 degree turn in both directions within a maximum diameter circle of 19.1 meters as measured at the outer sidewall of the front tire with the CTIS pressure as specified in 3.1.1.6.5. The transmission shall be in first gear, 8X4 wheel drive and the engine at minimum idle speed.

Specifications No. 2017.11 through 2017.20

Date: 12 December 2017

3.1.1.6 Sustainability

3.1.1.6.1 Towing

The ICVV, at GVWR, shall be capable of unassisted towing and being towed on a level hard surface road with a tow bar by all Stryker configurations. The ICVV shall be equipped with towed vehicle service brakes that are controlled by the brakes of the towing Stryker. The ICVV vehicle shall be capable of safely performing towing at a minimum speed of 1.5 mph uphill and 30 mph downhill on

30% grades (given that the towed vehicle has a functioning brake system).

The ICVV shall be capable of safely towing a range of trailers from 3/4 ton up to a fully loaded

Palletized Loading System (PLS) trailers (50,000 lbs) and supporting 4,000 lb. tongue weight on the towing pintle. The ICVV shall be capable of controlling the trailers' service, emergency, and parking brakes. When coupled with the lunette trailers and with regard to the service, parking and emergency brakes, the combination braking system ("as delivered" on the ICVV in combination with air brakes on the trailer) shall hold the vehicle plus trailer combination motionless on a dry hard surface 30% grade when headed up or down grade.

3.1.1.6.2 Self Recovery

The ICVV shall have self-recovery capability by means of a winch with a continuous line pull after winch break in of 21,000-24,000 pounds with major hydraulic subsystems turned off. The usable length of wire rope shall be 150 feet measured from the exit point of the front fairlead.

3.1.1.6.3 NATO Slave Receptacle

The ICVV shall have a NATO slave start receptacle and slave start capability.

3.1.1.6.4 Fuel System

3.1.1.6.4.1 Fuel Shutoff

The ICVV shall have manual fuel shutoff capability. Shutoff valves shall be located within easy reach of driver and crew IAW MIL-STD-1472. Shutoff valves shall have protective covers to prevent accidental activation.

3.1.1.6.4.2 Fuel Scavenging.

The ICVV shall be capable of exporting fuel at a minimum of 0.7 gpm at +72°F/+22°C.

3.1.1.6.4.3 Fuel Leveling

The Stryker FoV shall be capable of cross leveling fuel between the two (2) onboard fuel tanks to maximize performance on slope if/when fuel levels are too low to provide proper flow to the engine, or if a tank is damaged in order to save remaining fuel.

3.1.1.6.5 Tire Inflation

The ICVV shall be equipped with Central Tire Inflation System (CTIS), run-flat tires and shall provide the capability to remove and change tires without additional resources or assistance from outside sources. The CTIS shall inflate tires for multiple configurations IAW Table 3 below; supporting multiple tire loads.

Table 3: CTIS Controller Settings

Maximum Load per

Tire

Highway

(up to 60 MPH)

Cross Country

(up to 45 MPH)

Mud/Snow

(up to 20 MPH)

Emergency

(up to 10 MPH)

8500 lbs (Circle) 80 PSI 42 PSI 24 PSI 20 PSI

9000 lbs (Star) 89 PSI 56 PSI 28 PSI 23 PSI

9700 lbs (Square) 98 PSI 62 PSI 34 PSI 27 PSI

CTIS pressures have a range of +/- 3 psig

Pressures assume Michelin 395/85R20 XML or equivalent tires at all eight wheel stations

3.1.1.6.6 Fuel and Lubrication

The ICVV shall use all the fuels of Commercial Item Descriptio