Maritime-Motor_DRAFT_SRD_ACC.pdf

FOR OFFICIAL USE ONLY

System Requirements Document (SRD)

For Guardian Angel Maritime Recovery System

(Motors)

December 2014

Released by the

Battlefield Airmen Branch AFLCMC/WISN Air Force Life Cycle Management Center

Wright-Patterson Air Force Base OH 45433-7200

DISTRIBUTION A: APPROVED FOR PUBLIC RELEASE; DISTRIBUTION IS

UNLIMITED.

INFORMATION CONCERNING THE BATTLEFIELD AIRMEN PROGRAM

SHALL BE REFERRED TO AFLCMC/WISN BATTLEFIELD AIRMEN BRANCH

1895 FIFTH STREET, BUILDING 46,

WRIGHT-PATTERSON AFB OH 45433-7200.

LOCAL REPRODUCTION AUTHORIZED

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SUBMITTED BY

PAUL J. HROSCH, GS-14, DAF Date Chief Engineer, Battlefield Airmen Branch

AFLCMC/WISN

CONCURRENCE

ANGELO F. PIETRANTONIO, GS-14, DAF Date Chief, Battlefield Airmen Branch

AFLCMC/WISN

COMPONENT APPROVAL

WILLIAM G. YOUNG, GS-14, DAF Date Acting Chief, A5R PR Weapons Systems Division

HQ ACC/A5RG

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Revision History

Date Revision Description Prepared by:

1.0 Executive Summary

1.1.1 Concept of Employment

1.1.2 Concept of Operations (CONOPS)

2.0 Reference Documents

3.0 System Requirements

3.1 Submersible Motor

4.0 Verification Provisions

5.0 Definitions and Acronyms

Table 1 Verification Cross Reference Matrix (VCRM)

1.0 Executive Summary

Guardian Angel (GA) is organized, trained, and equipped to provide a rapid response to search, rescue, and recovery operations during peacetime, wartime, and overseas contingency operations. GA is unique in that it can respond to almost every situation during which an isolated personnel requires rescue and/or equipment needs recovery. Through deliberate and crisis action planning, GA teams organize and select the equipment and tactics necessary to accomplish the mission in threat environments across the range of geographic and environmental conditions. This includes, but is not limited to the airborne insertion of teams and equipment to locate an isolated person (IP) and/or sensitive equipment and relocation to a defensible recovery site if needed.

Guardian Angel (GA) forces are tasked to perform Combat Search and Rescue (CSAR) and Personnel Recovery (PR) operations in harsh maritime environments. In situations where isolated personnel (IP) face immediate threats to life, the range, speed, and threat limitations of vertical-lift aircraft dictate the employment of mission-unique airdrop capable watercraft from fixed wing aircraft. The existing limitations of the current outboard engines directly impact GAs ability to provide continuous support to the Combatant Commands (COCOMs), and meet all current taskings in support of worldwide isolated personnel and/or sensitive equipment recovery in maritime conditions. Currently, teams tasked to perform maritime alert missions are working with interim solutions and antiquated equipment. GA has difficulty operating in sea states generated by greater than Beaufort rating of 3, putting potential recovery missions at risk.

Failure to address these capability gaps by finding a long term sustainable engine, which is capable of operating in sea states caused by winds above 10 knots, will result in a degradation of capability to recover IP and/or sensitive equipment from maritime environments. To address this capability shortfall, GA requires the acquisition procurement of a propulsion system that overcomes the capability gaps. GA requires fielding and retrofitting of 165 submersible engines.

1.1 Concept of Employment and Operations Summary

1.1.1 Concept of Employment

GA forces are tasked to perform Personnel Recovery and Recovery Operations (PR/RO) to include Casualty Evacuation Sensitive Item Recovery and CSAR, across the full Range of Military Operations (ROMO) for maritime operations. GA forces must be capable of recovery operations in riverine, flooded areas, small bodies of water, and coastal environments. GA forces require a motor with the appropriate configuration/capabilities to effectively execute missions in these environments .

1.1.2 Concept of Operations (CONOPS)

To meet all mission requirements across the ROMO and environments, GA forces require a motor capable of propelling a craft transporting up to 1500 lbs at minimum speeds of 15 knots or greater. This maritime configuration/employment method is required to conduct maritime rescue operations in riverine, flooded areas, and in small bodies of water, and coastal environments.

2.0 Reference Documents

• Guardian Angel Maritime Recovery Increment I, Boat and Motor, Requirements Document

(RD), 21 April 2014.

• INTERIM, TO 13C7-51-21 Air Drop of Supplies and Equipment: Rigging Loads for

Special Operations. (n.d.)

• AFI 16-1202 Tethered Duck procedures.

• 40 CFR Part 91 Control of Emissions from Marine spark-ignition engines

• MILITARY STANDARD 810G (MIL-STD-810G)w/ Change 1, TEST METHOD

STANDARD ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND

LABORATORY TESTS, 15 April 2014.

3.0 System Requirements

Engines shall meet all requirements listed below in fresh and salt water.

3.1 Submersible Motor

3.1.1 Engine shall propel craft with 1500 lbs payload at a minimum speed of 15 kts in

Beaufort rating of 3 (T) should propel craft with 2000 lbs payload at a minimum speed of 10 kts in Beaufort rating of 5 (O).

3.1.2 After a minimum submersion of 10 ft for 10 min (T=O), the operator shall have the ability to purge water from the system and restart within 10 minutes (T) should have the ability to purge water from system and restart within 5 minutes (O).

Rationale: RAMZ package difficulties have caused motors to be submersed. This requirement provides a safety factor for the accidental submersion of the motor and covers an intentional sinking of the craft in certain mission sets.

3.1.3 Engine while mounted to the boat must be air deployable from rotary-wing platform (when configured as a package with a boat) in order to facilitate helicopter (HH-60G) deployments IAW AFI 16-1202 Tethered Duck procedures.

(T=O)

3.1.4 Engine while mounted to the boat must be air deployable from fixed-wing platform (M/HC-130P/N/J, C-130/C-130J, KC-130J and C-17 aircraft) when rigged IAW INTERIM, TO 13C7-51-21 Air Drop of Supplies and Equipment:

Rigging Loads for Special Operations. (n.d.)

3.1.5 Engine while mounted to the boat must fit within the dimensions of the RAMZ package. Refer to: INTERIM TO 13C7-51-21 Air Drop of Supplies and Equipment: Rigging Loads for Special Operations (n.d.) (pages 1 -15).

3.1.6 Engine shall be started and operable by one (1) person. (T=O)

3.1.7 Engine shall be able to use Gas or Diesel (T) multi-fuel. (O)

-- Note: Multi-fuel, engines must be able to meet all performance parameters with diesel, JP 5/8, Jet A, Kerosene, and 87 to 93 Octane gas.

3.1.8 Engine shall have manual backup starting method (e.g.. the rope can be manually re-routed). (T)

-- Repair kit shall include an extra manual start device in case of breakage.

3.1.9 The engine shall be capable of storage for 120 days with day time temperatures ranging from -50 degrees F to 130 degrees F (T) and -50 degrees F to 160 degrees F. (O)

3.1.10 The engine shall be capable of operating in water temperatures from 30 degrees F to 100 degrees. (T=O)

3.1.11 Engine shall not weigh more than 175 lbs (T), should not weigh more than 150 lbs. (O)

3.1.12 Engine shall withstand being packed in RAMZ configuration (90 degrees) for periods up to 4 months (T) and 6 months (O) without leaking oil/fluids or degradation of operational capability.

3.1.13 Propulsion system fouling shall be clearable without specialized equipment in an open ocean environment within 5 minutes. (T=O)

3.1.14 Engine shall have an external fuel bladder system with quick disconnect fittings.

(T=O)

3.1.15 The Engine shall have a subdued non-reflective color. (T=O)

-- Acceptable subdued, non-reflective colors for engines are black and/or gray.

3.1.16 Engine shall be field repairable. (T=O)

3.1.17 Engine shall have National Marine Manufacture Association Certification and adheres to 40 CFR Part 91 Control of Emissions from Marine spark-ignition engines. (T=O)

3.1.18 Engine should be comprised of non-corroding material. (O)

3.1.19 Engine shall comply with relevant sections of MIL-STD 810G for worldwide operations. (T)

4.0 Verification Provisions

4.1 Verification methods.

4.1.1 Demonstration.

Operation of the system, subsystem or a part of the system that relies on observable, functional operation, not requiring use of instrumentation, special test equipment or subsequent analysis.

4.1.2 Test.

Operation of the system, subsystem or a part of the system using instrumentation or other special test equipment to collect data for later analysis.

4.1.3 Analysis.

Processing of accumulated data obtained from other qualification methods. Examples are reduction interpolation or extrapolation of test results.

4.1.4 Inspection.

Visual examination of system components, documentation, etc.

Table 1 Verification Cross Reference Matrix (VCRM)

Item Analysis Inspection Demo Test

3.1.1 Engine shall propel craft with 1500 lbs

payload at a minimum speed of 15 kts in Beaufort rating of 3 (T) should propel craft with 2000 lbs payload at a minimum speed of 10 kts in Beaufort rating of 5. (O)

X

3.1.2 After a minimum submersion of 10 ft for

10 min (T=O), the operator shall have the ability to purge water from the system and restart within 10 minutes (T) should have the ability to purge water from system and restart within 5 minutes.

(O)

X

3.1.3 Engine must be air deployable from rotary-

wing platform (when configured as a package with a boat) in order to facilitate helicopter (HH- 60G) deployments IAW AFI 16-1202 Tethered Duck procedures. (T=O)

SS X

3.1.4 Engine while mounted to the boat must be

air deployable from fixed-wing platform (M/HC- 130P/N/J, C-130/C-130J, KC-130J and C-17 aircraft) when rigged IAW INTERIM, TO 13C7- 51-21 Air Drop of Supplies and Equipment: Rigging Loads for Special Operations. (n.d.)

3.1.5 Engine must fit within the dimensions of the

RAMZ package. Refer to: INTERIM TO 13C7-51-21 Air Drop of Supplies and Equipment: Rigging Loads for Special Operations (n.d.) (pages 1 -15).

X

Item Analysis Inspection Demo Test

3.1.6 Engine shall be started and operable by one

(1) person. (T=O) X

3.1.7 Engine shall be able to use Gas or Diesel

(T) multi-fuel. (O) X

3.1.8 Engine shall have manual backup starting

method (e.g.. the rope can be manually re-routed).

(T) X

3.1.9 The engine shall be capable of storage for

30 days with day time temperatures ranging from -50 degrees F to 130 degrees F (T) and -50 degrees F to 160 degrees F. (O)

X/SS

3.1.10 The engine shall be capable of operating

in water temperatures from 30 degrees F to 100 degrees. (T=O)

X/SS

3.1.11 Engine shall not weigh more than 175 lbs

(T), should not weigh more than 150 lbs. (O) X

3.1.12 Engine shall withstand being packed in

RAMZ configuration (90 degrees) for periods up to 4 months (T) and 6 months (O) without leaking oil/fluids or degradation of operational capability

X/SS

3.1.13 Propulsion system fouling shall be

clearable without specialized equipment in an open ocean environment within 5 minutes. (T=O)

X

3.1.14 Engine shall have an external fuel bladder

system with quick disconnect fittings. (T=O) X

3.1.15 The Engine shall have a subdued non-

reflective color. (T=O) X

3.1.16 Engine shall be field repairable. (T=O) X

3.1.17 Engine shall have National Marine

Manufacture Association Certification and adheres to 40 CFR Part 91 Control of Emissions from Marine spark-ignition engines. (T=O)

X

3.1.18 Engine should be comprised of non-

corroding material. (O) X/A

3.1.19 Engine shall comply with relevant

sections of MIL-STD 810G for worldwide operations. (T)

X/SS

5.0 Definitions and Acronyms

Definitions Payload (3.1.1): 1500 lbs is inclusive of people, fuel, and gear

Field repairable (3.1.13): Ability to repair engine (Replace starter cord and spark plug(s)) with onboard repair kit.

Acronyms

AF Air Force COCOM Combatant Commander CONOPS Concepts of Operations CSAR Combat Search And Rescue GA Guardian Angel IAW In Accordance With MSDS material safety data sheets O Objective PR Personnel Recovery RAMZ Rigging Alternate Method Zodiac ROMO Range of Military Operations SCUBA Self-Contained Underwater Breathing Apparatus SRD System Requirements Document T Threshold T-Duck Tethered Duck VCRM Verification Cross Reference Matrix