RIF_2016_Amendment_0003.pdf

DOD Rapid Innovation Fund – Amendment 0003 1

DoD Rapid Innovation Fund FY 2016 – Amendment 0003

Number: HQ0034-16-BAA-RIF-0001 The purpose of Amendment 0003 to the DoD Rapid Innovation Fund FY2016 Broad Agency Announcement, HQ0034-16-BAA-RIF-0001 is to add three requirements, provide clarification to three existing requirements, and to make corrective changes to the solicitation.

Important Note: The following changes have been made to this solicitation since Amendment 2 was released — April 2, 2016.

Annex Text Changes

Within Section 13.2 Department of the Army Annex:

The following three new requirements are added:

Requirement # ARMY57-PEOCSS10:

Title: Modernized Ambulance Compartment with improved HVAC system Military System or Acquisition Program Customer: PEO CS&CSS / PD Light Tactical Vehicles Description: The existing fleet of Army ambulances, excluding the M997A3 are more than two decades old. The age has created obsolesce and degradation issues that may require a future recapitalization effort. Technology advancements over the last two decades have been significant, and as a result, there exists an opportunity to improve the performance and reliability capabilities with commercial items in the M997 series. Future recapitalization would utilize the M1097A2 chassis. Technology insertion with commercial items in the ambulance is of interest to the Army. This includes, but is not limited to, and improved HVAC system, litter carriers, LED lighting, sealing of the compartment, electrical outlet integration, refrigeration, and rear door improvements. The combination of cost-effective solution and improved capabilities is desired for the future recapitalization of the M997.

Technical Point of Contact: Clifton Ellis, (586) 381-3519, Clifton.s.ellis.civ@mail.mil

Requirement Number# ARMY58-PEOCSS11:

Title: Anti-lock Braking System / Electronic Stability Control (ABS/ESC) for non-armored versions of the High Mobility Multipurpose Wheeled Vehicle (HMMWV) Military System or Acquisition Program Customer: PEO CS&CSS / PD Light Tactical Vehicles Description: The HMMWV has been in military service for more than 3 decades, and has seen its mission evolve significantly. Through those years the HMMWV has incorporated 1000s of changes, but the rapid advancement of commercial technology has left gaps in capability for older portions of the HMMWV fleets. Specifically, the M1097A2 has not incorporated ABS/ESC as a feature despite the mandate from FMVSS in 2011 for US Auto Manufacturers.

There is a need to integrate a militarized ABS/ESC to the M1097A2.

Technical Point of Contact: Clifton Ellis, (586) 381-3519, Clifton.s.ellis.civ@mail.mil mailto:Clifton.s.ellis.civ@mail.mil

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Requirement Number# ARMY59-PEOCSS12:

Title: Airbag / Airbelt integration in the HMMWV:

Military System or Acquisition Program Customer: PEO CS&CSS / PD Light Tactical Vehicles Description: American forces rely on vehicle performance both on and off-road to carries out a variety of missions. These missions include, but are not limited to, disaster relief, homeland security, training and overseas operations. These diverse environments require a wide range of performance parameters for vehicles to operate within. As technology has matured, it has created opportunities to fill existing capability gaps and improve vehicle performance and safety. There is a need to improve on and off-road vehicle safety with the integration of improved restraints and airbelts to the High Mobility Multipurpose Wheeled Vehicle (HMMWV). The combination of a cost-effective commercial technology in a military environment will aid in reducing occupant injuries in HMMWV accidents.

Technical Point of Contact: Clifton Ellis, (586) 381-3519, Clifton.s.ellis.civ@mail.mil

Within Section 13.4 Department of the Air Force Annex:

Requirement # 9.a:

Technical POC, the telephone number for Maj Andrew Soine has changed to read: 937-255-

Within Section 13.5 Office of the Secretary of Defense (OSD) / Defense Agencies Annex:

Requirement # ASDR&E-16-BAA-RIF-ARL-HPO-0001:

Technical POC, the telephone number for Dr. Guy French has changed to read 937-713-7030

Annex Requirement Clarifying Information

Within Section 13.3 Department of the Navy Annex:

The following information is provided as clarification to the requirement published in the BAA:

Requirement # FY16-DoN-RIF-NAVAIR-10:

1. The dosimetry system is envisioned to be used by both Flight Deck Personnel and Aircrew. As such the dosimeter must be compatible with the HGU-84, HGU-68, HGU- 56 and HGU-24P. If the recording device is wearable, it must not interfere with assigned

DOD Rapid Innovation Fund – Amendment 0003 3 crew or maintenance duties and be fully interoperable with Aircrew Life Support Systems and Personal Protective Equipment.

2. The primary intent of this RIF is to obtain the capability to measure in-ear noise while aircrew or flight deck crews perform their mission. In addition, the capability to measure noise external to the helmet is desired for determining effectiveness of hearing protection and/or assess noise environment. This capability should be modular. The external dosimeter should be capable of use with the In-ear dosimetry system or stand alone.

3. The system should be able to operate in the following environments - Mil-Std 464 , Mil-

Std 461 and Mil-Std 810.

4. The dosimetry system must have the capability to load recorded data on a standalone storage device. Eventually, the data may be cloud stored, but security requirements at this time would add a level of complexity that would exceed RFI timeline. The monitor must be able to record a minimum of 8hrs of data with the objective of 12hrs. The storage device must be able to store data for multiple crews for at least 6 months.

5. The on deck noise environment :

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Within Section 13.4 Department of the Air Force Annex:

Requirement # 4.o:

The current systems referred to the in topic 4.o are Joint Mobile IRCM Test System (JMITS) and the Multi-Spectral Sea and Land Target Simulator (MSALTS). The attached document provides additional information on these two systems.

Joint Mobile IRCM Test System (JMITS)

Background

1. Provides the ability to test installed system on aircraft in open air environment

2. Transportable ground Based Missile Plume Simulator (2 complete systems)

a. Simultaneous UV and dual-color IR

3. IRCM response characterization

4. Extensive Near-Real Time & Post-Mission Analysis Capability

5. Self-sufficient

Capabilities

1. Simultaneous UV and dual color IR missile simulation

a. Current MANPAD threats as well as some vehicle-launched threats

b. Near real-time atmospheric and emitter degradation correction

c. Downrange radiometric suite for calibration and atmospheric correction

2. IRCM response characterization

a. Jam beam laser characterization (20 calibrated radiometers)

3. 4 centerline, 16 off-axis banded radiometers

a. Static Seeker Capability

4. Supports flare effectiveness assessments and jam response

5. Up to 4 static seekers, roll fixtures to support rolling seeker bodies

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6. Precision pointing and tracking

a. Day and night tracking, Range-Only-Radar

7. Radar supports real time correction of signature amplitude based on actual slant ranges

8. Dynamic Slant Range Correction

a. Predicts aircraft path based on JMITS tracking measurements to provide a more accurate slant range value for correcting generated signature outputs to match desired simulation

9. Flex Play - ability to proactively manage test execution by

a. Automatically firing planned simulations based on positive aircraft position feed back (vs. relying on position “mark calls”)

b. Automatically selecting and firing the most appropriate simulation for the current aircraft position (KTM Az/El feedback and slant range) and flight parameters (computed track)

10. Quick-look assessments

a. Performed during mission with summary at end of the mission

b. Simulation quality, KTM track quality and CM response assessment

11. Post-mission/post-test data analysis and reporting

a. Jam laser performance and expendable effectiveness

b. Tracking performance (requires A/C TSPI)

c. Simulation desired vs. achieved signature analysis

12. Standardized processes and methodologies used throughout JMITS

a. Validated signature generation using MSIC approved models (TMAP, EMSIG) and the Standardized Missile Simulation Methodology

b. JTAMS calibration and measurements standards applied

c. Standardized data analysis processes used (jam beam analysis and seeker responses)

d. Instruments and radiometers calibrated on regular intervals

Multi-Spectral Sea and Land Target Simulator (MSALTS)

Background

1. Mobile IRCM missile simulator

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a. Simultaneous UV and dual-color IR

2. Ability to simulate missile firings while moving

a. Mobility helps overcome ground referenced spatial limitations of stationary ground simulators

3. Portable and Mobile

a. Capable of supporting multiple test locations in one day

4. Land and sea capable

a. Simulator pallet adaptable to either truck or QST-35B target boat

b. Other mounting configurations are possible

5. CTEIP funded, three units being procured

6. Final delivery of last system expected by end of FY16

Capabilities

1. MSALTS has the same or upgraded capabilities of JMITS, except for static seekers and no off-axis radiometers

a. Simultaneous UV and dual color IR validated missile simulations

b. Downrange radiometric suite for calibration and atmospheric correction

c. IRCM laser response characterization (3 calibrated radiometers)

d. Dynamic slant range correction

e. Flex-play

f. Precision pointing and tracking

g. Quick-look assessments (throughout the mission)

h. Post-mission/post-test data analysis and reporting

2. Contained in much smaller footprint with true mobility between and during engagements and ability to deploy at sea

3. Same processes and methodologies as JMITS, with common data products between the two systems

Requirement # TRANSCOM-16-BAA-RIF-0001:

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The proposed solution will meet the following Key System Attributes:

Solid Oxide Fuel Cell (SOFC) Key Performance Parameters (KPPs) KPP# Key System Attribute (KSA) Threshold Objective

K100 Construction Ruggedized Ruggedized K101 Individual case weight Single case 35lbs or less Single case 25lbs or less K102 Transport Man-portable Man-portable K103 Operate on common tactical fuels Diesel, DF2, JP-5, JP-8 Diesel, DF2, JP-5, JP-8 K104 Power output 1.2Kw @ 29 VDC

(combined up to 2 units) 1.2Kw @ 29VDC (single unit)

K105 Exposure to vibration Conforms to MIL-STD- 810G, Method 514.6 Procedure I

Conforms to MIL-STD- 810G, Method 514.6 Procedure I

K106 Acoustic noise Conforms to MIL-STD- 810G, Method 515.6

Conforms to MIL-STD- 810G, Method 515.6

K107 Exhaust and Environmental Conforms to MIL-STD- 810G

Conforms to MIL-STD- 810G

K108 Heat signature Conforms to MIL-STD- 810G

Conforms to MIL-STD- 810G

K109 Environmental operational paramenter

-20 to +50 degrees C -40 to +60 degrees C

K110 Interoperability / Scalability Current military power generating equipment and alternative energy sources (Solar, wind, etc.) and Stackable (Load sharing) with same model unit(s)

Current military power generating equipment and alternative energy sources (Solar, wind, etc.) and Stackable (Load sharing) with same model unit(s)

K111 Serviceability/Maintenance interval

1,000 Hrs. minimun scheduled service / 3,000 Hrs. Depot overhaul

1,000 Hrs. minimun scheduled service / 3,000 Hrs. Depot overhaul