CHMD_PP_Conference_ldl_062617.pdf

Project Manager Soldier WarriorProject Manager Soldier Warrior

Our Strength and PurposeOur Strength and Purpose

Common Helmet Mounted Display (CHMD)

27 June 2017

Larry Lucas

Product Manager Air Warrior

HGU-56/P RWH

Rotary Wing Helmet

• Advanced See-Through, High-Definition, Digital Helmet Mounted Display (HMD) System that Overlays Symbology and Allows the Aviator to View Flight Parameters without Looking Down at the Aircraft’s Instrumentation

• Supports Army Rotary Wing Platforms

• Replaces Current Heads Up Display (HUD)

• Will Integrate with HGU-56/P RWH that is Modified with Magnetic Head Tracker and other Head Borne Aviation Life Support Equipment (ALSE)

• Will become part of the Air Soldier Modular Integrated Helmet and Display System (MIHDS), Helmet Display and Tracking System (HDTS)

Common Helmet Mounted Display (CHMD)

SECTION C – PRODUCTION STATEMENT OF WORK

• Describes the efforts required for production of the Air Soldier Common Helmet Mounted Display (CHMD)

• PM AW plans to procure a Non Developmental Item (NDI) display capable of satisfying the Air Soldier System CHMD requirements, Support Equipment, Repair Parts, and Carrying Case hardware items in addition to post production support

• Includes the completion of First Article Test (FAT) and the delivery of Logistics product data for training and provisioning

• Also includes provisions for Teardown, Inspect, Repair and Return (TIRR) capability

SECTION M – EVALUATION FACTORS FOR AWARD

3.0 TECHNICAL/SYSTEM PERFORMANCE FACTOR

3.1) Compliance matrix Performance Sub-factor ref. Section J, attachment 20

3.2) Systems Integration and Test Sub-factor

4.0 PRODUCTION FACTOR

4.1) Manufacturing Sub-factor

4.2) Functional Support Sub-factor

5.0 PRICE/COST FACTOR

5.1) Hardware Price Subfactor

5.2) System Integration and Qualification and Post Production Support Cost Subfactor

5.3) Projected Life-Cycle Sustainment Cost Subfactor

6.0 PAST PERFORMANCE FACTOR

7.0 SMALL BUSINESS FACTOR

Factors and Relative Rankings:

Technical/System Performance Factor

Sub-factors:

Production Factor

Sub-Factors:

Price/Cost Factor

Sub-Factors:

Past Performance Factor

No Sub-factors:

Small Business Factor

No Sub-factors:

Technical/ System Performance

Production Price/ Cost

Past Performance

Small Business

Compliance Matrix - Qualification

Manufacturing Functional Support

Systems Integration and Test

Hardware Price (CHMD and Carrying Case)

Projected Life- Cycle

Sustainment Cost

Integration and Test Activities Cost (CPFF)

Priority Requirements

3.1.3.1 CHMD see-through Display

3.1.3.2 CHMD Day/Night Operation

3.3.3 System Resolution

3.3.4 FOV

3.3.7 Eye Box

3.3.8 Latency

3.3.14 ANVIS Alignment

3.3.15 Flicker/Jitter

3.6.1.1 Operating Requirements-Temperature

3.6.1.3 Operating Requirements Altitude

3.6.8 *Combined Environmental Effects

3.6.10 *Vibration

3.6.11 *Explosive Atmosphere

3.6.12.1.1 *CE101

3.6.12.1.2 *CE102

3.6.12.1.3 RE101

3.6.12.1.4 *RE102

3.6.12.2.1 CS101

3.6.12.2.2 CS114

3.6.12.2.3 CS115

3.6.12.2.4 CS116

3.6.12.2.5 RS101

3.6.12.2.6 RS103

3.6.13 ESD

All Priority Requirements are Weighted Equally

Safety of Flight Requirements are Marked with an Asterisk

Generic Requirements

3.1.1 Weight 3.6.6 Humidity

3.2 Marking & Identification 3.6.7 Fungus

3.3.1.1 D65 3.6.9.1 Transit Drop Shock

3.3.1.2 Visible Spectrum 3.7.1.1 MTBF

3.3.1.3 P43 3.7.1.2 MTTR

3.3.2 Color 3.7.1.3 Maintenance Ratio

3.3.5 Luminance 3.7.2.1 Special Tools/Support Equipment

3.3.5.1 Day Luminance (inside the visor) 3.7.2.2 Aviation Maintenance Concept

3.3.5.2 Day Luminance (outside the visor) 3.7.2.3 Army Organic Maintenance System

3.3.5.3 Night Luminance (outside the visor) 3.8.1 System Safety

3.3.6.1 White Contrast to the Eye 3.8.2 Health Hazards

3.3.6.2 Red Contrast to the Eye 3.8.3 Human Factors Engineering

3.3.6.3 Green Contrast to the Eye 3.8.3.1 Physical Eye Relief

3.3.9 Focus 3.8.3.3 Inadvertent Activation

3.3.10 Combiner Prismatic Deviation 3.8.3.4 Donning and Doffing

3.3.11 Combiner Refractive Power 3.8.3.5 Cold Flyer Glove

3.3.12 Combiner Optical Distortion 3.8.3.6 Incorrect Connectivity

3.3.13 Combiner Haze 3.8.3.8 5th-95th Percentile Accommodation

3.3.16 CHMD Luminance Uniformity 3.8.3.8.1 Fore / Aft adjustment

3.3.17 CHMD Linear Distortion 3.8.3.8.2 IPD adjustment

3.3.18 CHMD Field Curvature 3.8.3.8.3 Vertical Adjustment

3.3.19 CHMD Contrast Transfer Function (CTF) 3.9.1 Resistance to Battlefield Contaminan

3.5.1.1 Tool Free Mounting

3.5.1.3 QDC capability

3.6.1.2 Transport/Storage Temperature

3.6.1.4 Transport(Non Operational) Altitude

3.6.1.5 Temperature Shock

3.6.2 Blowing Dust

3.6.3 Dripping Rain

3.6.4 Blowing Sand

3.6.5 Salt Fog

First Article and Workmanship Requirements (3.10.1, 3.10.2, 3.10.3, 3.10.4, and 3.11) are Not Listed in this Document

Generic and Integration Requirements are Not Listed in Order of Importance

Integration Requirements

3.1.2.1 Center of Mass (Neck Fatigue)

3.1.2.2 Center of Mass (Neck Injury)

3.1.4.1 Impact Protection, Crown & Headband

3.1.4.2 Impact Protection Ear

3.3.20 Day/Night Transition

3.4 Night Vision Compatibility

3.5.1.2 Stow/Deploy

3.5.1.4 CHMD Compatibility with Visors (Day Configuration)

3.5.1.5 Non-Interference with ALSE Equipment

3.5.1.6 ANVIS Compatibility

3.5.1.7 ANVIS Look Around Capability

3.5.1.8 ANVIS Attribute Compatibility

3.5.1.9 ANVIS Operation with Failed CHMD

3.5.2 ASDC Interface

3.5.3 Non-Interference with Helmet Tracker Kit (HTK)

3.6.12.3 *EMC

3.6.12.4 *EMV

3.8.3.2 Crash Injury Risk

3.8.3.7 *Ingress/Egress

3.8.3.9 Signatures

Use of Government Labs, Facilities, Hardware, and Aircraft may be Required to Complete Integration Requirements

Integration Requirements may be Completed after Contract Award

Safety of Flight Requirements are Marked with an Asterisk

Generic and Integration Requirements are Not Listed in Order of Importance

SECTION L – PROPOSAL SUBMISSION

• Volume I Title: Technical/System Performance; Two hardcopies; two CDs (Technical/System Performance submission); Total Pagecount: 100

• Volume II Title: Production Factor: Two hardcopies; two CDs; Page Count: 50

• Volume III Title: Price/Cost Factor; Two hardcopies; two CDs; Page Count:

As Required

• Volume IV Title: Past Performance Factor; Two hardcopies; two CDs; Page Count: 50

• Volume V Title: Small Business Factor; Two hardcopies; two CDs; Page Count: As Required

• Volume VI Title: Administrative Matters; Two hardcopies; two CDs; Page Count: As Required

VATEP

Objectives

CHMD

Specification Paragraph

Maximum

VATEP %

Reduction in

CLIN 0001

Proposed Price

Calculation of VATEP % Identify where in offeror’s proposal the VATEP objective is met

Field of View

3.3.4 5% Objective is binary. An offerors proposal will either meet or fail to meet the objective. The offeror’s proposal for CHMD shall provide a field of view, at a physical eye relief of 25mm, equal to or greater than 30º vertical by 40º horizontal with 50º diagonal.

CHMD

Type:

Single Display

3.1.3.2 4% Objective is binary. An offerors proposal will either meet or fail to meet the objective. The offeror’s proposal for CHMD type shall support both day and night operations with a single display.

System Resolution

3.3.3 2% Objective is binary. An offerors proposal will either meet or fail to meet the objective. The offeror’s proposal for CHMD shall provide a system resolution of ≥18 cycles/deg.

CHMD

Type:

Switchable

3.1.3.1 1% Objective is binary. An offerors proposal will either meet or fail to meet the objective. The offeror’s proposal for CHMD type shall be switchable to either eye or biocular.