Attach_0013_Work_Breakdown_Structure-Cost_and_Software_Data_Report_Plan_31Jan2018.pdf

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

W31P4Q-19-X-XXXX

Attachment #0013

31 January 2018

WBS # Level 1 Level 2 Level 3 Level 4 Level 5 Definition

1.0 Hydra-70 Ordnance

System

The complex of hardware, software, data, services, and facilities required to develop and produce the capability for applying munitions to a target.

Includes, for example:

a. Wings and fins that provide aerodynamic flight control in response to electro-mechanical signals and are attached to the munition body

b. Structural body assemblies including the structure, covers, skins, adhesives, and fairings not directly applicable to any other Level 3 munition subsystem

c. Protection devices for stressing environmental conditions such as thermal protection system or rain erosion that are not directly applicable to other Level 3 munition subsystems

1.1 Munition

Historically, munitions were unguided weapons unpowered after leaving its launching device that has as its purpose the destruction of some object or target.

1.1.1 Airframe

This element comprises the structural framework that provides the aerodynamic shape, mounting surfaces and environmental protection for the munition components, which are not directly applicable to other specific Level 3 munition subsystems.

1.1.2 Propulsion - MK66

The element comprises the equipment integral to the munition, which provides supplemental forces post launch to propel the munition from its launch position to the target or to assist in countering the forces of drag (i.e., base bleed). The equipment may employ solid rocket motor or air-breathing technologies.

1.1.2.1 Hydra 70 (covers army items below

denoted with AUR)

The structure (integral to the propulsion system), propellant, controls, instrumentation, and all other installed subsystem equipment integral to the rocket motor or engine as an entity within itself.

1.1.2.1.1 Rocket Motor Integration, Load, Assembly, Pack, Test and Checkout

This element includes the load, assembly and packing of the MK66 Mod4 rocket motor at the contractor facility and includes integration, assembly, inspection and checkout of the complete rocket motor ready to integrate with warheads fro Army All Up Rounds.

1.1.2.1.2 Rocket Motor Grain

The structure (integral to the propulsion system), propellant, controls, instrumentation, and all other installed subsystem equipment integral to the rocket motor or engine as an entity within itself.

Rocket Motor. This element is applicable to a solid propulsion system and consists of the thrust producing component in which solid propellant, made up of fuel and oxidizer, is combusted and expelled through a nozzle. It includes the pressure vessel, an igniter, internal insulation, solid propellant and a nozzle. If applicable it includes the functionality to move the nozzle or a portion of the nozzle but not the actuation system to cause that movement.

1.1.2.1.3 Rocket Motor Tube

The motor tube supports the other components of the rocket. Presently, all motor tubes are aluminum, threaded internally at the front end for warhead installation, and grooved or threaded internally at the aft end for nozzle and fin assembly installation. The Mk 66 Mods rocket motor tube is an integral bulkhead type of motor tube and is impact-extruded from aluminum stock.

1.1.2.1.4 Nozzle/Fin Assembly

This element includes the nozzle assembly for the Mk 66 and consists of the nozzle body, carbon insert, fins, contact band assembly, and weather seal. The steel nozzle body expansion cone has flutes that cause the rocket to spin during free flight.

1.1.2.1.5 Stabilizing Rod

This element is comprised of the stabilizing rod, located in the perforation of the motor propellant grain, is salt coated to prevent unstable burning of the propellant. It also reduces flash and after burning in the rocket motor, which could contribute to compressor stall and flameout of the aircraft jet engines.

When the propellant ignites, the stabilizing rod ensures that the grain ignites simultaneously forward and aft.

1.1.2.1.6 Rocket Motor Igniter

The igniter heats the propellant grain to ignition temperature. The igniter used in the 2.75-inch motor is a disc-shaped metal container that contains a black powder and magnesium charge, a squib, and electrical lead wires. It is located at the forward end of the motor.

1.1.2.2 Air Force (used as GFE for AF

programs)

The structure (integral to the propulsion system), propellant, controls, instrumentation, and all other installed subsystem equipment integral to the rocket motor or engine as an entity within itself.

1.1.2.2.1 Rocket Motor Integration, Load, Assembly, Pack, Test and Checkout

This element includes the load, assembly and packing of the MK66 Mod4 rocket motor at the contractor facility and includes integration, assembly, inspection and checkout of the complete rocket motor ready to ship.

1.1.2.2.2 Rocket Motor Grain

The structure (integral to the propulsion system), propellant, controls, instrumentation, and all other installed subsystem equipment integral to the rocket motor or engine as an entity within itself.

Rocket Motor. This element is applicable to a solid propulsion system and consists of the thrust producing component in which solid propellant, made up of fuel and oxidizer, is combusted and expelled through a nozzle. It includes the pressure vessel, an igniter, internal insulation, solid propellant and a nozzle. If applicable it includes the functionality to move the nozzle or a portion of the nozzle but not the actuation system to cause that movement.

1.1.2.2.3 Rocket Motor Tube

The motor tube supports the other components of the rocket. Presently, all motor tubes are aluminum, threaded internally at the front end for warhead installation, and grooved or threaded internally at the aft end for nozzle and fin assembly installation. The Mk 66 Mods rocket motor tube is an integral bulkhead type of motor tube and is impact-extruded from aluminum stock.

18 January 2018

1.1.2.2.4 Nozzle/Fin Assembly

This element includes the nozzle assembly for the Mk 66 and consists of the nozzle body, carbon insert, fins, contact band assembly, and weather seal. The steel nozzle body expansion cone has flutes that cause the rocket to spin during free flight.

1.1.2.2.5 Stabilizing Rod

This element is comprised of the stabilizing rod, located in the perforation of the motor propellant grain, is salt coated to prevent unstable burning of the propellant. It also reduces flash and after burning in the rocket motor, which could contribute to compressor stall and flameout of the aircraft jet engines.

When the propellant ignites, the stabilizing rod ensures that the grain ignites simultaneously forward and aft.

1.1.2.2.6 Rocket Motor Igniter

The igniter heats the propellant grain to ignition temperature. The igniter used in the 2.75-inch motor is a disc-shaped metal container that contains a black powder and magnesium charge, a squib, and electrical lead wires. It is located at the forward end of the motor.

1.1.2.3 Navy (used as GFE for Navy

programs)

The structure (integral to the propulsion system), propellant, controls, instrumentation, and all other installed subsystem equipment integral to the rocket motor or engine as an entity within itself.

1.1.2.3.1 Rocket Motor Integration, Load, Assembly, Pack, Test and Checkout

This element includes the load, assembly and packing of the MK66 Mod4 rocket motor at the contractor facility and includes integration, assembly, inspection and checkout of the complete rocket motor ready to ship.

1.1.2.3.2 Rocket Motor Grain

Rocket Motor. This element is applicable to a solid propulsion system and consists of the thrust producing component in which solid propellant, made up of fuel and oxidizer, is combusted and expelled through a nozzle. It includes the pressure vessel, an igniter, internal insulation, solid propellant and a nozzle. If applicable it includes the functionality to move the nozzle or a portion of the nozzle but not the actuation system to cause that movement.

1.1.2.3.3 Rocket Motor Tube

The motor tube supports the other components of the rocket. Presently, all motor tubes are aluminum, threaded internally at the front end for warhead installation, and grooved or threaded internally at the aft end for nozzle and fin assembly installation. The Mk 66 Mods rocket motor tube is an integral bulkhead type of motor tube and is impact-extruded from aluminum stock.

1.1.2.3.4 Nozzle/Fin Assembly

This element includes the nozzle assembly for the Mk 66 and consists of the nozzle body, carbon insert, fins, contact band assembly, and weather seal. The steel nozzle body expansion cone has flutes that cause the rocket to spin during free flight.

1.1.2.3.5 Stabilizing Rod

This element is comprised of the stabilizing rod, located in the perforation of the motor propellant grain, is salt coated to prevent unstable burning of the propellant. It also reduces flash and after burning in the rocket motor, which could contribute to compressor stall and flameout of the aircraft jet engines.

When the propellant ignites, the stabilizing rod ensures that the grain ignites simultaneously forward and aft.

1.1.2.3.6 Rocket Motor Igniter

The igniter heats the propellant grain to ignition temperature. The igniter used in the 2.75-inch motor is a disc-shaped metal container that contains a black powder and magnesium charge, a squib, and electrical lead wires. It is located at the forward end of the motor.

1.1.3 Power and Distribution This element is not applicable to the Hydra-70 contract.

1.1.4 Guidance This element is not applicable to the Hydra-70 contract.

1.1.5 Navigation This element is not applicable to the Hydra-70 contract.

1.1.6 Controls This element is not applicable to the Hydra-70 contract.

1.1.7 Communications This element is not applicable to the Hydra-70 contract.

1.1.8 Payload - Warhead

1.1.8.1 HA13 (M274) All Up Round (AUR) Smoke Signature Practice Warhead All Up Round Hydra 70

1.1.8.1.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and signal payload. This element also includes the integration of the payload with the rocket motor for a complete AUR munition.

1.1.8.1.2 Warhead Materials/Mechanism

The M274 body consists of two main parts, the nose and the base, which are welded (brazed) together. The bulk of the lethality is obtained from the nose section which is fabricated using nodular, pearlitic malleable cast iron.

1.1.8.1.3 Smoke Signal Explosive Compound

The Smoke compound for the M274 consists of a cylindrical cartridge assembly is in the forward section of the casing; it contains approximately 2 ounces of potassium perchlorate and aluminum powder that provides a "flash, bang, and smoke" signature.

1.1.8.1.4 Fuze - M423 Upon acceleration of the rocket at firing, a weight setback occurs in the unbalanced rotor assembly which houses the primer and detonator.

This setback places the fuze into an armed condition .

1.1.8.1.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.2 H872 (M274) Warhead Only Smoke Signature Practice Warhead Only

1.1.8.2.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and signal payload.

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

Attachment #0013

31 January 2018

1.1.8.2.2 Warhead Materials/Mechanism

The M274 body consists of two main parts, the nose and the base, which are welded (brazed) together. The bulk of the lethality is obtained from the nose section which is fabricated using nodular, pearlitic malleable cast iron.

1.1.8.2.3 Smoke Signal Explosive Compound

The Smoke compound for the M274 consists of a cylindrical cartridge assembly is in the forward section of the casing; it contains approximately 2 ounces of potassium perchlorate and aluminum powder that provides a "flash, bang, and smoke" signature.

1.1.8.2.4 Fuze - M423

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.2.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.3 HA18 (M257) AUR Battlefield Illumination Warhead All Up Round Hydra 70

1.1.8.3.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and illumination payload. This element also includes the integration of the payload with the rocket motor for a complete AUR munition.

1.1.8.3.2 Warhead Materials/Mechanism

The M257 illuminating flare consists of a main parachute, drogue parachute assembly and an integral fuze and delay assembly. The warhead is enclosed in an aluminum case.

1.1.8.3.3 Flare Payload This element consists of an ignition system, and candle flare

1.1.8.3.4 Fuze - M442

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.3.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.4 H812 (M257) Warhead Only Battlefield Illumination Warhead Only

1.1.8.4.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and illumination payload.

1.1.8.4.2 Warhead Materials/Mechanism

The M257 illuminating flare consists of a main parachute, drogue parachute assembly and an integral fuze and delay assembly. The warhead is enclosed in an aluminum case.

1.1.8.4.3 Flare Payload This element consists of an ignition system, and candle flare

1.1.8.4.4 Fuze - M442

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.4.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.5 HA10 (M278) AUR Battlefield I/R Illumination Warhead All Up Round Hydra 70

1.1.8.5.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and illumination payload. This element also includes the integration of the payload with the rocket motor for a complete AUR munition.

1.1.8.5.2 Warhead Materials/Mechanism

The M278 illuminating flare consists of a main parachute, drogue parachute assembly and an integral fuze and delay assembly. The warhead is enclosed in an aluminum case.

1.1.8.5.3 Illumination Flare Payload This element consists of an ignition system, and candle flare

1.1.8.5.4 Fuze - M442

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.5.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.6 HA06 (M278) Warhead Only Battlefield I/R Illumination Warhead Only

1.1.8.6.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and illumination payload.

1.1.8.6.2 Warhead Materials/Mechanism

The M278 illuminating flare consists of a main parachute, drogue parachute assembly and an integral fuze and delay assembly. The warhead is enclosed in an aluminum case.

1.1.8.6.3 IR Flare Payload This element consists of an ignition system, and candle flare

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

1.1.8.6.4 Fuze - M442

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.6.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.7 HA76 (M156) AUR White Phosphorus Smoke Warhead All Up Round Hydra 70

1.1.8.7.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and signal payload. This element also includes the integration of the payload with the rocket motor for a complete AUR munition.

1.1.8.7.2 Warhead Materials/Mechanism

The M156 body consists of two main parts, the nose and the base, which are welded (brazed) together. The bulk of the lethality is obtained from the nose section which is fabricated using nodular, pearlitic malleable cast iron.

1.1.8.7.3 White Phosphorus Payload This element is the white phosphorus filler for the M156 which also contains a small bursting charge of composition B to open the warhead on impact.

1.1.8.7.4 Fuze - M423

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.7.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.8 H855 (M156) Warhead Only White Phosphorus Smoke Warhead Only

1.1.8.8.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and signal payload.

1.1.8.8.2 Warhead Materials/Mechanism

The M156 body consists of two main parts, the nose and the base, which are welded (brazed) together. The bulk of the lethality is obtained from the nose section which is fabricated using nodular, pearlitic malleable cast iron.

1.1.8.8.3 White Phosphorus Payload This element is the white phosphorus filler for the M156 which also contains a small bursting charge of composition B to open the warhead on impact.

1.1.8.8.4 Fuze - M423

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.8.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.9 HA23 (WTU-1/B) Navy Only Inert Navy Practice Warhead Only

1.1.8.9.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload.

1.1.8.9.2 Warhead Materials/Mechanism The WTU-1/b uses a cast iron warhead that is similar in shape and weight to the M151 Warhead

1.1.8.9.3 Inert Payload The payload is made up of cast iron.

1.1.8.9.4 Fuze N/A No fuze is used for the inert round.

1.1.8.9.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.10 RESERVED

1.1.8.10.1 RESERVED

1.1.8.10.2 RESERVED

1.1.8.10.3 RESERVED

1.1.8.10.4 RESERVED

1.1.8.10.5 RESERVED

1.1.8.11 HA72 (M282) Warhead Only Multi Purpose Penetrator Warhead Only

1.1.8.11.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and high explosive payload.

1.1.8.11.2 Warhead Materials/Mechanism

The M282 casing consists of metal parts. The bulk of the lethality is obtained from the nose section which is fabricated using nodular, pearlitic malleable cast iron.

1.1.8.11.3 High Explosive Payload The high explosive payload compound.

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

1.1.8.11.4 Fuze M423

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.11.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.12 HA12 (M151) AUR High Explosive Point Detonation All Up Round Hydra 70

1.1.8.12.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and high explosive payload. This element also includes the integration of the payload with the rocket motor for a complete AUR munition.

1.1.8.12.2 Warhead Materials/Mechanism

The M151 body consists of two main parts, the nose and the base, which are welded (brazed) together. The bulk of the lethality is obtained from the nose section which is fabricated using nodular, pearlitic malleable cast iron.

1.1.8.12.3 High Explosive Payload The high explosive payload consists 2.3 pounds (1.04 kg) of composition B-4 High Explosive (HE).

1.1.8.12.4 Fuze M423

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.12.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.13 HA09 (M229) AUR High Explosive Point Detonation All Up Round Hydra 70

1.1.8.13.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and high explosive payload. This element also includes the integration of the payload with the rocket motor for a complete AUR munition.

1.1.8.13.2 Warhead Materials/Mechanism

The M229 is an elongated version of the M151 body consists of two main parts, the nose and the base, which are welded (brazed) together. The bulk of the lethality is obtained from the nose section which is fabricated using nodular, pearlitic malleable cast iron.

1.1.8.13.3 High Explosive Payload The high explosive payload consists 4.8 pounds (2.18 kg) of composition B-4 High Explosive (HE).

1.1.8.13.4 Fuze M423

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.13.5 Other

This element comprises the unique fuzing and or warhead characteristics that are unanticipated at this time, but may become necessary with any applicable changes to the munition or fuzing components.

1.1.8.14 HA11 (M255A1) AUR Flechette Warhead All Up Round Hydra 70

1.1.8.14.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and expulsion payload. This element also includes the integration of the payload with the rocket motor for a complete AUR munition.

1.1.8.14.2 Warhead Materials/Mechanism

This warhead uses many standard components with the other cargo warheads, such as the plastic nose cone, aluminum case, umbilical cable, and the M439 Fuze

1.1.8.14.3 Flechette Payload This element is comprised of 1,179 60-grain flechettes

1.1.8.14.4 Fuze M439

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.14.5 Other - Umbilical

The Umbilical enables "smart fuzing" of the target defeat mechanism hardware and is an integral part of the M439 fuze used to determine the timing after launch to determine detonation.

1.1.8.15 HA50 (Mk149) Warhead Only Flechette Warhead Only

1.1.8.15.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and expulsion payload.

1.1.8.15.2 Warhead Materials/Mechanism

This warhead uses many standard components with the other cargo warheads, such as the plastic nose cone, aluminum case, umbilical cable, and the M439 Fuze

1.1.8.15.3 Flechette Payload This element is comprised of 1,179 60-grain flechettes

1.1.8.15.4 Fuze M439

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.15.5 Other - Umbilical

The Umbilical enables "smart fuzing" of the target defeat mechanism hardware and is an integral part of the M439 fuze used to determine the timing after launch to determine detonation.

1.1.8.16 HA15 (M264) AUR Red Phosphorus Smoke Warhead All Up Round Hydra 70

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

1.1.8.16.1 Payload Integration, Load, Assembly, Pack, Test and Checkout

This element consists all technical functions associated with payload integration, including the load, assembly, pack and inspection of the payload, integration of the fuze and signal payload. This element also includes the integration of the payload with the rocket motor for a complete AUR munition.

1.1.8.16.2 Warhead Materials/Mechanism

This warhead uses many standard components with the other cargo warheads, such as the plastic nose cone, aluminum case, umbilical cable, and the M439 Fuze

1.1.8.16.3 Red Phosphorus Smoke Payload This payload element is comprised of f red phosphorus used for smoke generation

1.1.8.16.4 Fuze M439

The equipment in the munition that controls the capability of initiating the TDM (e.g., mechanical, hydrostatic, inertial, counters, and timers). It includes the hardware and software for the Safe, Arm and Fire (SAF) function; sensors and algorithms, if applicable, to enable "smart fuzing"; and the hardware and software associated with the firing train.

1.1.8.16.5 Other - Umbilical

The Umbilical enables "smart fuzing" of the target defeat mechanism hardware and is an integral part of the M439 fuze used to determine the timing after launch to determine detonation.

1.1.9 On Board Test Equipment This element is not applicable to the Hydra-70 contract.

1.1.10 On Board Training Equipment This element is not applicable to the Hydra-70 contract.

1.1.11 Auxiliary Equipment This element is not applicable to the Hydra-70 contract.

1.1.12 Munition Software Release 1…n This element is not applicable to the Hydra-70 contract.

1.1.13 Munition Integration, Assembly, Test and Checkout

This element includes all effort of technical and functional activities associated with the design, development, and production of mating surfaces, structures, equipment, parts, materials, interconnect harnessing and software required for the integration, assembly and checkout of the Level 3 elements below into their Level 2 element, Munitions.

1.2 Encasement Device This element is not applicable to the Hydra-70 contract.

1.3 Launch System This element is not applicable to the Hydra-70 contract.

1.4 Ordnance System Software Release 1…n This element is not applicable to the Hydra-70 contract.

1.5 Ordnance System Integration, Assembly, Test and Checkout

This element includes all effort of technical and functional activities associated with the design, development, and production of mating surfaces, structures, equipment, parts, materials, interconnect harnessing and software required for the integration, assembly and checkout of the above Level 2 elements into their Level 1 element, Ordnance System.

1.6 System Engineering The technical and management efforts of directing and controlling a totally integrated engineering effort of a system or program.

1.7 Program Management

The business and administrative planning, organizing, directing, coordinating, controlling, and approval actions designated to accomplish overall program objectives, which are not associated with specific hardware elements and are not included in systems engineering.

1.8 System Test and Evaluation This element is not applicable to the Hydra-70 contract.

1.9 Training This element is not applicable to the Hydra-70 contract.

1.10 Data The deliverable data required to be listed on a contract data requirements list, DD Form 1423.

1.10.1 Technical Publications This element is not applicable to the Hydra-70 contract.

1.10.2 Engineering Data This element is not applicable to the Hydra-70 contract.

1.10.3 Management Data

The data items necessary for configuration management, cost, schedule, contractual data management, program management, etc., required by the Government.

Includes, for example:

a. Contractor cost reports, cost performance reports, contract funds status reports, schedules, milestones, networks, integrated support plans

b. For sea systems; Expanded Ship Work Breakdown Structure (ESWBS), contract data requirements (988) element

1.10.4 Support Data This element is not applicable to the Hydra-70 contract.

1.10.5 Data Depository This element is not applicable to the Hydra-70 contract.

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

1.11 Peculiar Support Equipment

The design, development, and production of those deliverable items and associated software required to support and maintain the system or portions of the system while the system is not directly engaged in the performance of its mission, and which are not common support equipment.

Includes, for example:

a. Vehicles, equipment, tools, etc., used to fuel, service, transport, hoist, repair, overhaul, assemble, disassemble, test, inspect, or otherwise maintain mission equipment

b. Any production of duplicate or modified factory test or tooling equipment delivered to the Government for use in maintaining the system. (Factory test and tooling equipment initially used by the contractor in the production process but subsequently delivered to the Government will be included as cost of the item produced.)

c. Any additional equipment or software required to maintain or modify the software portions of the system Excludes, for example:

a. Overall planning, management and task analysis functions inherent in the Work Breakdown Structure element, systems Engineering/Program Management

b. Common support equipment, presently in the DoD inventory or commercially available, bought by the using command, not by the acquiring command

1.11.1 Test and Measurement Equipment This element is not applicable to the Hydra-70 contract.

1.11.2 Support and Handling Equipment

The deliverable tools and handling equipment used for support of the mission system.

Includes, for example:

a. Ground support equipment, vehicular support equipment, powered support equipment, non-powered support equipment, munitions material handling equipment, materiel handling equipment, and software support equipment (hardware and software)

1.11.2.1 PA151 Fastpack This element consist of the production of the PA151 Fastpack for packing and shipping and of the Hydra 70 All Up Rounds.

1.11.2.2 Wood Box (6 per) This element consists of the wood boxes used to ship AURs, warheads, and rocket motors (6 per box)

1.11.2.3 Wood Box (4 per) This element consists of the wood boxes used to ship AURs, warheads, and rocket motors (4 per box)

1.12 Common Support Equipment This element is not applicable to the Hydra-70 contract.

1.13 Operational/Site Activation This element is not applicable to the Hydra-70 contract.

1.14 Industrial Facilities

The construction, conversion, or expansion of industrial facilities for production, inventory, and contractor depot maintenance required when that service is for the specific system.

Includes, for example:

a. Equipment acquisition or modernization, where applicable

b. Maintenance of these facilities or equipment

c. Industrial facilities for hazardous waste management to satisfy environmental standards Excludes, for example:

a. Capital equipment

1.14.1 Construction/Conversion/Expansion The real estate and preparation of system peculiar industrial facilities for production, inventory, depot maintenance, and other related activities.

1.14.2 Equipment Acquisition or Modernization

The production equipment acquisition, modernization, or transferal of equipment for the particular system. This pertains to Government owned and leased equipment under facilities contract.

1.14.3 Maintenance (Industrial Facilities) The maintenance, preservation, and repair of industrial facilities and equipment.

1.15 Initial Spares and Repair Parts This element is not applicable to the Hydra-70 contract.

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

a. NAME:

Pre-A B X C-FRP X

A C-LRIP O&S

PROGRAM X

X

X

a. CWBS

DICTIONARY

d. DD 1921-2

(PCR)

f. SRDR

FORMATS

X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X

DD FORM 2794, MAY 2011 PREVIOUS EDITION IS OBSOLETE

COST AND SOFTWARE DATA REPORTING PLAN Form Approved OMB No. 0704-0188

b. PHASE/MILESTONE c. PRIME MISSION PRODUCT

The public reporting burden for this collection of information is estimated to average 8 hours per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing the burden, to Department of Defense, Executive Services Directorate (0704-0188). Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number.

PLEASE DO NOT RETURN YOUR COMPLETED FORM TO THE ABOVE ORGANIZATION.

2. WBS SYSTEM TYPE

1. MAJOR PROGRAM Hydra-70

3. SUBMISSION TYPE 4. CURRENT SUBMISSION

DATE (YYYYMMDD)

256-842-4971

6c. FAX NUMBER (Include Area Code)

256-876-6807

Ordnance System2.75-inch Family of Air-to-Ground Rockets

5. LAST APPROVED PLAN DATE

(YYYYMMDD)

20120511

INITIAL

CHANGE

6d. E-MAIL ADDRESS duncan.tovar@us.army.mil

Contractor TBD

6a. POINT OF CONTACT (POC) NAME AND ADDRESS (Include ZIP Code) Duncan Tovar, PEO Missiles and Space Joint Attack Munition Systems Project Office

SFAE-MSLS-JAMS-B-CA

Redstone Arsenal, AL 35898

RDT&E

PROCUREMENT

O&M

9c. APPROPRIATION

6b. TELEPHONE NUMBER (Include Area Code)

7. PLAN TYPE

CONTRACT (PRIME)

CONTRACT (SUB)

ii. DIVISION 9a. CONTRACTOR NAME/ADDRESS

i. PERFORMING ORGANIZATION

1.0

1.1.6 1.1.6

1.1.4 1.1.4

9b. CONTRACT NUMBER

TBD

b. CONTRACT/

SUBCONTRACT

12.

WBS REPORTING ELEMENTS

11. WBS ELEMENT CODE 13. REPORTS REQUIRED

(X if applicable)

a. PROGRAM/

CONTRACT/

SUBCONTRACT

8. PREPARING

ORGANIZATION

JAMS PO

10. APPROVED PLAN NUMBER

c. DD 1921-1

(FCHR)

e. DD 1921-4

(CSR)

DD 1921-3 (CBDR):

Guidance N/A

1.1.3 1.1.3 Power and Distribution N/A

1.1.7 1.1.7 Communications N/A

1.1.8 1.1.8 Payload - Warhead X

X

b. DD 1921

(CDSR)

XHydra 70 Ordnance System

Controls N/A

1.0

1.1.5 1.1.5 Navigation N/A

1.1.2 1.1.2.3.4 Nozzle/Fin Assembly X

1.1.2 1.1.2.3.5 Stabilizing Rod X

1.1.2 1.1.2.3.6 Rocket Motor Igniter X

1.1.2 1.1.2.3.1 Rocket Motor Integration, Load, Assembly, Pack, Test and Checkout X

1.1.2 1.1.2.3.2 Rocket Motor Grain X

1.1.2 1.1.2.3.3 Rocket Motor Tube X

1.1.2 1.1.2.2.5 Stabilizing Rod X

1.1.2 1.1.2.2.6 Rocket Motor Igniter X

1.1.2 1.1.2.3 Navy (used as GFE for Navy programs) X

1.1.2 1.1.2.2.2 Rocket Motor Grain X

1.1.2 1.1.2.2.3 Rocket Motor Tube X

1.1.2 1.1.2.2.4 Nozzle/Fin Assembly X

1.1.2 1.1.2.1.6 Rocket Motor Igniter X

1.1.2 1.1.2.2 Air Force (used as GFE for AF programs) X

1.1.2 1.1.2.2.1 Rocket Motor Integration, Load, Assembly, Pack, Test and Checkout X

1.1.2 1.1.2.1.3 Rocket Motor Tube X

1.1.2 1.1.2.1.4 Nozzle/Fin Assembly X

1.1.2 1.1.2.1.5 Stabilizing Rod X

1.1.2 1.1.2.1 Hydra 70 (covers army items below denoted with AUR) X

1.1.2 1.1.2.1.1 Rocket Motor Integration, Load, Assembly, Pack, Test and Checkout X

1.1.2 1.1.2.1.2 Rocket Motor Grain X

1.1 1.1 Munition X

1.1.1 1.1.1 Airframe X

1.1.2 1.1.2 Propulsion - MK-66 X

1.1.8 1.1.8.1.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.1 HA13 (M274) All Up Round (AUR) X

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

X

a. CWBS

DICTIONARY

d. DD 1921-2

(PCR)

f. SRDR

FORMATS

X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X

DD FORM 2794, MAY 2011 PREVIOUS EDITION IS OBSOLETE

X

11. WBS ELEMENT CODE

12.

WBS REPORTING ELEMENTS

13. REPORTS REQUIRED

(X if applicable) DD 1921-3 (CBDR):

a. PROGRAM/

CONTRACT/

SUBCONTRACT

b. CONTRACT/

SUBCONTRACT

b. DD 1921

(CDSR)

c. DD 1921-1

(FCHR)

e. DD 1921-4

(CSR)

1.1.8 1.1.8.9 HA23 (WTU-1/B) Navy Only X

1.1.8 1.1.8.9.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.1.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.8.3 White Phosphorus Payload X

1.1.8 1.1.8.8.4 Fuze - M423 X

1.1.8 1.1.8.8.5 Other X

1.1.8 1.1.8.8 H855 (M156) Warhead Only X

1.1.8 1.1.8.8.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.8.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.7.3 White Phosphorus Payload X

1.1.8 1.1.8.7.4 Fuze - M423 X

1.1.8 1.1.8.7.5 Other X

1.1.8 1.1.8.7 HA76 (M156) AUR X

1.1.8 1.1.8.7.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.7.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.6.3 IR Flare Payload X

1.1.8 1.1.8.6.4 Fuze - M442 X

1.1.8 1.1.8.6.5 Other X

1.1.8 1.1.8.6 HA06 (M278) Warhead Only X

1.1.8 1.1.8.6.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.6.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.5.3 Ilumination Flare Payload X

1.1.8 1.1.8.5.4 Fuze - M442 X

1.1.8 1.1.8.5.5 Other X

1.1.8 1.1.8.5 HA10 (M278) AUR X

1.1.8 1.1.8.5.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.5.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.4.3 Flare Payload X

1.1.8 1.1.8.4.4 Fuze - M442 X

1.1.8 1.1.8.4.5 Other X

1.1.8 1.1.8.4 H812 (M257) Warhead Only X

1.1.8 1.1.8.4.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.4.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.3.3 Flare Payload X

1.1.8 1.1.8.3.4 Fuze - M442 X

1.1.8 1.1.8.3.5 Other X

1.1.8 1.1.8.3 HA18 (M257) AUR X

1.1.8 1.1.8.3.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.3.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.2.3 Smoke Signal Explosive Compound X

1.1.8 1.1.8.2.4 Fuze - M423 X

1.1.8 1.1.8.2.5 Other X

1.1.8 1.1.8.2 H872 (M274) Warhead Only X

1.1.8 1.1.8.2.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.2.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.1.3 Smoke Signal Explosive Compound X

1.1.8 1.1.8.1.4 Fuze - M423 X

1.1.8 1.1.8.1.5 Other X

11. WBS ELEMENT CODE

12.

13. REPORTS REQUIRED

(X if applicable) DD 1921-3 (CBDR):

1.1.8 1.1.8.9.3 Inert Payload X

1.1.8 1.1.8.9.2 Warhead Materials/Mechanism X

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

a. CWBS

DICTIONARY

d. DD 1921-2

(PCR)

f. SRDR

FORMATS

X X

X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X

DD FORM 2794, MAY 2011 PREVIOUS EDITION IS OBSOLETE

X

a. CWBS

DICTIONARY

d. DD 1921-2

(PCR)

f. SRDR

FORMATS

WBS REPORTING ELEMENTSa. PROGRAM/

CONTRACT/

SUBCONTRACT

b. CONTRACT/

SUBCONTRACT

b. DD 1921

(CDSR)

c. DD 1921-1

(FCHR)

e. DD 1921-4

(CSR)

1.1.11 1.1.11 Auxiliary Equipment N/A

1.1.12 1.1.12 Munition Software Release 1...n N/A

1.1.8 1.1.8.9.4 Fuze N/A X

1.1.8 1.1.8.16.5 Other - Umbilical X

1.1.9 1.1.9 On Board Test Equipment N/A

1.1.10 1.1.10 On Board Training Equipment N/A

1.1.8 1.1.8.16.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.16.3 Red Phosprus Smoke Payload X

1.1.8 1.1.8.16.4 Fuze M439 X

1.1.8 1.1.8.15.5 Other - Umbilical X

1.1.8 1.1.8.16 HA15 (M264) AUR X

1.1.8 1.1.8.16.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.15.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.15.3 Flechette Payload X

1.1.8 1.1.8.15.4 Fuze M439 X

1.1.8 1.1.8.14.5 Other - Umbilical X

1.1.8 1.1.8.15 HA50 (Mk149) Warhead Only X

1.1.8 1.1.8.15.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.14.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.14.3 Flechette Payload X

1.1.8 1.1.8.14.4 Fuze M439 X

1.1.8 1.1.8.13.5 Other X

1.1.8 1.1.8.14 HA11 (M255A1) AUR X

1.1.8 1.1.8.14.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.13.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.13.3 High Explosive Payload X

1.1.8 1.1.8.13.4 Fuze M423 X

1.1.8 1.1.8.12.5 Other X

1.1.8 1.1.8.13 HA09 (M229) AUR X

1.1.8 1.1.8.13.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.12.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.12.3 High Explosive Payload X

1.1.8 1.1.8.12.4 Fuze M423 X

1.1.8 1.1.8.11.5 Other X

1.1.8 1.1.8.12 HA12 (M151) AUR X

1.1.8 1.1.8.12.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.11.2 Warhead Materials/Mechanism X

1.1.8 1.1.8.11.3 High Explosive Payload X

1.1.8 1.1.8.11.4 Fuze X

1.1.8 1.1.8.10.5 RESERVED

1.1.8 1.1.8.11 HA72 (M282) Warhead Only X

1.1.8 1.1.8.11.1 Payload Integration, Load, Assembly, Pack, Test and Checkout X

1.1.8 1.1.8.10.2 RESERVED

1.1.8 1.1.8.10.3 RESERVED

1.1.8 1.1.8.10.4 RESERVED

1.1.8 1.1.8.9.5 Other X

1.1.8 1.1.8.10 RESERVED

1.1.8 1.1.8.10.1 RESERVED

11. WBS ELEMENT CODE

12.

WBS REPORTING ELEMENTS

13. REPORTS REQUIRED

(X if applicable) DD 1921-3 (CBDR):

a. PROGRAM/

CONTRACT/

SUBCONTRACT

b. CONTRACT/

SUBCONTRACT

b. DD 1921

(CDSR)

c. DD 1921-1

(FCHR)

e. DD 1921-4

(CSR)

1.2 1.2 Encasement Device N/A

1.1.13 1.1.13 Munition Integration, Assembly, Test and Checkout X

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

X X X X X X X X X X X X X X X X X X X X X X X X X

DD FORM 2794, MAY 2011 PREVIOUS EDITION IS OBSOLETE

1.3 1.3 Launch System N/A

Total Price X

Reporting Contractor Profit/Loss or Fee X

Reporting Contractor Management Reserve X Reporting Contractor FCCM X Total Cost X

Reporting Contractor G&A X Reporting Contractor Undistributed Budget X

1.15 1.15 Initial Spares and Repair Parts N/A

Subtotal Cost X

1.14.1 1.14.1 Construction/Conversion/Expansion X

1.14.2 1.14.2 Equipment Acquisition or Modernization X

1.14.3 1.14.3 Maintenance (Industrial Facilities) X

1.12 1.12 Common Support Equipment N/A

1.13 1.13 Operational/Site Activation N/A

1.14 1.14 Industrial Facilities X

1.11.2 1.11.2.1 PA151 Fastpack X

1.11.2 1.11.2.2 Wood Box (6 per) X

1.11.2 1.11.2.3 Wood Box (4 per) X

1.11 1.11 Peculiar Support Equipment X

1.11.1 1.11.1 Test and Measurement Equipment N/A

1.11.2 1.11.2 Support and Handling Equipment X

1.10.3 1.10.3 Management Data X

1.10.4 1.10.4 Support Data N/A

1.10.5 1.10.5 Data Depository N/A

1.10 1.10 Data X

1.10.1 1.10.1 Technical Publications N/A

1.10.2 1.10.2 Engineering Data N/A

1.7 1.7 Program Management X

1.8 1.8 System Test and Evaluation N/A

1.9 1.9 Training N/A

1.4 1.4 Ordnance System Software Release 1...n N/A

1.5 1.5 Ordnance System Integration, Assembly, Test and Checkout X

1.6 1.6 System Engineering X

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

d. AS OF DATE e. DUE DATE

(YYYYMMDD) (YYYYMMDD)

1 CWBS Dictionary Contract Award 20140331 20140531 2 1921, 1921-1 Initial Report Contract Award 20140331 20140531 3 1921, 1921-1 Final Delivery Base 20160930 20161130 4 1921, 1921-1 Final Delivery Option Year 1 20170930 20171130 5 1921, 1921-1 Final Delivery Option Year 2 20180930 20181130 6 1921, 1921-1 Final Delivery Option Year 3 20190930 20191130 7 1921, 1921-1 Final Delivery Option Year 4 20200930 20201130

DD FORM 2794 (PAGE 2), MAY 2011 PREVIOUS EDITION IS OBSOLETE

14. CSDR SUBMISSION DATES

15. REMARKS

c.

EVENT

a.

SUBMISSION

b.

FORM(S)

1. DD Form 1921-3 (CBDR): The DD Form 1921-3 is a mandatory requirement for all prime contractors and subcontractors performing work on contracts which contain CSDR requirements. As such, the contractor must ensure that its FPR business entity submits a completed DD Form 1921-3 within 60 days subsequent to the end of the contractor's fiscal year. Only one DD Form 1921-3 submission is required per FPR business entity, independent of the number of contracts with CSDR requirements held by the business entity. This is not a contract-specific deliverable. The contractor must ensure that the requirement is being fulfilled at the FPR business level while any CSDR requirements are being fulfileed at a contract level.

2. Non-Recurring/Recurring Definitions: The contractor will utilize the specific definitions and requirements in the CSDR Manual (DoD 5000.04-M-1) and the definitions in the DIDs for the DD Forms 1921 and 1921-1 to segregate recurring and nonrecurring costs. Refinements or expansions to these definitions are TBD pending the post contract award conference.

3. Cost Accounting Standards (CAS) Disclosure Statement Differences: The contractor will complete the 1921 reports by complying with the company's CAS disclosure statement . The CAS Disclosure Statement will be reviewed during the post contract award conference to include addressing the need for mapping from the contractor's accounting system into the required contractor cost data reporting (CCDR) functional categories.

WORK BREAKDOWN STRUCTURE - COST AND SOFTWARE DATA REPORT PLAN

31 January 2018 (Draft)

a. NAME:

Pre-A B X C-FRP

A C-LRIP O&S

PROGRAM X

X

X

a. CWBS

DICTIONARY

d. DD 1921-2

(PCR)

f. SRDR

FORMATS

X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X

DD FORM 2794, MAY 2011 PREVIOUS EDITION IS OBSOLETE

1.1.8.2.10.1 1.1.8.2.10.2

M255A1 Flechette Warhead (Cargo) M255A2 Flechette Warhead Night Reliability Indicator (NRI) (Cargo)

X X

X

b. DD 1921

(CDSR)

XHYDRA 70 ROCKET SYSTEM

Fuze X X

1.01.0

1.1.8.4

b. CONTRACT/

SUBCONTRACT

12.

WBS REPORTING ELEMENTS

11. WBS ELEMENT CODE 13. REPORTS REQUIRED

(X if applicable)

a. PROGRAM/

CONTRACT/

SUBCONTRACT

10. APPROVED PLAN NUMBER

c. DD 1921-1

(FCHR)

e. DD 1921-4

(CSR)

DD 1921-3 (CBDR):

9b. CONTRACT NUMBER

6d. E-MAIL ADDRESS

TBD

6a. POINT OF CONTACT (POC) NAME AND ADDRESS (Include ZIP Code)

RDT&E

PROCUREMENT

O&M

9c. APPROPRIATION

6b. TELEPHONE NUMBER (Include Area Code)

7. PLAN TYPE

CONTRACT (PRIME)

CONTRACT (SUB)

ii. DIVISION 9a. CONTRACTOR NAME/ADDRESS

i. PERFORMING ORGANIZATION

8. PREPARING

ORGANIZATION

COST AND SOFTWARE DATA REPORTING PLAN Form Approved OMB No. 0704-0188

b. PHASE/MILESTONE c. PRIME MISSION PRODUCT

The public reporting burden for this collection of information is estimated to average 8 hours per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information.