16 Ton Class Manned
Ground Vehicle
BIA
Number: 15000
Pricing
Information
The
LSI anticipates a funding level of approximately $775,000 for each
contract award(s) resulting from this BIA.
Detailed
Description of Effort and Task
The
Future Combat System (FCS) manned ground vehicle plan is for a family
of approximately fifteen different combat vehicles based on a common
platform that is compatible with transporting and fielding in a combat
ready configuration on a C-130 military air transport without a transportation
waiver restriction (except the NLOS, BLOS, and mortar vehicle which
are expected to exceed the nominal 16 short ton weight). This limits
the combat ready weight of each vehicle. Each vehicle is distinct
when equipped and assembled with a unique mission module system consisting
of a combination of carrier and/or ordnance systems. All components
will be based on an open system architecture and facilitate block
upgrades spiral development throughout the life of the vehicle.
This Statement
of Work (SOW) is applicable for system level integration of the 16
ton class FCS manned ground vehicles in Table I. We are requesting
proposals for the period of performance October 7 through December
20, 2002, for the integrated vehicle design refinement to a level
to support an early PDR in SDD, the subsystem design interface work
required to integrate these vehicles, and the associated system level
specification development support for developing the specifications.
The integrator
is responsible for integrating both the common subsystems and the
unique mission subsystems that is required for each of the vehicles
defined in Table I. The integrator will provide support in the development
of the vehicle level specifications by the LSI. The integrator will
be responsible for the subsystem specifications, common and unique.
The vehicle integrator will provide draft/legacy subsystem specifications
for review. Potential common subsystems reside in the following areas;
chassis-hull, mobility system, ECS/TMS/NBC systems, survivability
systems, vetronics, warfighter machine interface, AutoNav, communication
system, and the sensors.
Key factors
to be considered for integrating each vehicle system include C-130
deployability and weight control, reliability, maintainability, and
supportability. Design features that reduce logistics footprint and
improve operability will also improve cost benefit.
Weight
is a critical design attribute that will make the vehicles capable
components of the FCS system of systems architecture. We are interested
in a description of the weight allocation, tracking, and mitigation
plan for meeting the weight requirement for each concept. We are interested
in any weight reductions that have been introduced, applied, or can
be applied to meet performance and weight goals.
Low Life-Cycle-Cost
is important to making FCS successful. That makes maintainability,
supportability and reliability attributes also vital points of interest
to us. Extended operation without re-supply, cross platform part commonality,
and reduced logistics footprint are additional points of interest.
Please provide a description of your plan to exceed legacy attributes
and characteristics at the major system/subsystem level in these areas
with cost savings in mind.
|
TABLE
I - Unique Vehicle Mission Module Subsystems and Attributes
|
| |
Vehicle
System
|
Attributes
and Technology
|
| T1 |
LOS/BLOS |
Vehicle
Combat vehicle with 105-120mm cannon with LOS/BLOS capability.
Also included is a Self Protection Weapon. |
| T2 |
NLOS
Cannon Vehicle |
Combat
vehicle with 120-155mm cannon with NLOS capability. This system
incorporates technologies that include CARGO rounds and smart
submunitions, and Fire and Forget Seeker technology. Also included
is a Self Protection Weapon. |
| T3 |
NLOS
Mortar Vehicle |
Combat
vehicle with 120mm mortar gun with NLOS capability. Also included
is a Self Protection Weapon. |
| T4
|
Missiles
Vehicle |
Combat
vehicle carries missiles-in-a-box configuration that minimizes
reloading time and effort. The Missile system provides BLOS precision
guided missiles and loitering munitions. Also included is a Self
Protection Weapon. |
| T5 |
Armored
Personnel Carrier |
Transports
a full 9-man infantry squad including their associated gear and
2 soldier crew. Also included is a Self Protection Weapon. |
| T6 |
Control
Vehicle (CV) |
Provides
4 soldier workstation, 1 driver and 1 commander. Used for control
of UGV's andUAV's. Also included is a Self Protection Weapon.
|
| T7 |
Command
and Control (C2) Vehicle |
Provides
4 soldier workstation, 1 driver and 1 commander. Provides the
connection among the Force and communication on the move. Also
included is a Self Protection Weapon. |
| T8 |
Re-supply
Vehicle |
General-purpose
vehicle with embedded semi-autonomy provides operation as a follower.
Crew size consists of 1 driver and 1 commander. Also included
is a Self Protection Weapon. |
| T9 |
Reconnaissance,
Surveillance, and Target Acquisition (RSTA) Vehicle |
Integrates
RSTA suite of 5-meter mast, thermal imagers (LWIR and MWIR), day/night
TV camera, 10 km+ laser range finder, Ka band radar, and 360 deg.
all elevation azimuth. Provides 2 soldier workstation, 1 driver
and 1 commander. Also included is a Self Protection Weapon. |
| T10 |
155
mm Re-supply Vehicle |
Provides
automated re-supply to the 155-mm NLOS vehicle; re-supplied with
palletized ammunition: Crew size consists of 1 driver and 1 commander.
Also included is a Self Protection Weapon. |
| T11 |
Recovery
Vehicle |
Provides
towing and recovery assistance. Crew size consists of 1 driver
and 1 commander. Also included is a Self Protection Weapon. |
| T12 |
Medical
Vehicle |
Vehicle
provides evacuation and/or medical treatment. Provides 1 injured
station, 1 driver and 1 commander. |
| T13 |
Bridge
Vehicle |
Equipped
to lay bridge. |
| T14 |
Mobility/Countermobility
Vehicle |
Equipped
to breach and lay minefields, can be operated semi-autonomously;
mission package includes a scraper, flail, and Mongoose. Vehicle
has semi-autonomous capability. Also included is a Self Protection
Weapon. |
| T15 |
SUAV
Launcher Carrier Vehicle |
Transports
a pod of 32 SUAV's and the launching system. Crew size consists
of 1 driver and 1 commander. |
Task
1
Coordinate
the major system level requirements and define major Interface Control
Documents (ICD) with LSI. A Platform architecture shall be developed
for each variant that defines the internal relationships among subsystem
components as well as the relationships between to the C4ISR architecture.
Initial system requirements, architecture and assumptions will be
provided at the start of the contract. On going trade studies and
refinement of the Operational Requirements Document (ORD) may require
updates to initial requirements and/or vehicle systems defined in
Table I.
Task
2
Refine
the concept design from the Concept Technology Development (CTD) phase
1 to a level that will support an early PDR (to be announced later)
during the SDD phase. This may include some refinement of existing
completed trade study work from phase 1 CTD. Define vehicle-to-subsystem-to-subsystem
interfaces to a level to demonstrate major transport element routing.
Provide
top-level description of the major vehicle subsystems. Descriptions
shall include schematics/block diagrams, top-level performance characteristics,
growth potential to support spiral upgrades, weight, RAM-D, cost,
etc.
Provide
rationale used to arrive at system/subsystem design requirements.
Provide
assessments or compliance with these requirements and architecture
definitions provided by the LSI.
Task
3
Provide
3D CAD Envelope Models and 2D Layouts of the system general arrangement
locating the major system elements sufficient to define subsystem-to-vehicle
interfaces. The choice is for 3D CAD Envelope Model datasets to be
either PRO/Engineer version 2001 or CATIA V4. If not available in
either of these CAD formats a STEP format file shall submitted. 2D
layouts to be contractor CAD dataset format and one 36" wide paper
plot. Provide simulation model of system performance to support vehicle
performance simulation assessments.
- EASY5
or MATLAB/Simulink for system level analyses
- DADS
or equivalent at a minimum COTS software for multi-body dynamic
analysis (DADS is preferred).
Task
4
Provide
subsystem commonality plan that maximizes commonality across all vehicle
systems. Plan shall include at a minimum: proposed common subsystem(s)
for each vehicle system listed in Table I. Also, for each vehicle
in Table I, provide the following for each common subsystem: (1) ROM
vehicle non-recurring and recurring cost delta (+/-$), (2) ROM vehicle
weight delta (+/-lbs) and (3) any other potential pro/cons (i.e. maintenance,
survivability, mobility, etc.). Provide functional schematics depicting
the integration of common subsystems and mission unique subsystems
for each vehicle system in Table I. Provide ROM vehicle subsystem
requirements for: heating /cooling, power (electrical, hydraulic,
pneumatic), and durability and reliability predictions.
Task
5
Support
the development and creation of vehicle-to-C4ISR, vehicle-to-supportability,
and vehicle-to-training ICDs..
Task
6
Provide
preliminary SDD program plan, based on LSI provided key milestones,
to include at a minimum: preliminary system element development/verification
plan (i.e., describe a top-level plan for vehicle testing that would
correlate predictions of subsystem, and a fully integrated vehicle),
preliminary system manufacturing plan, long lead items list, program
critical path, preliminary subsystem/vehicle system level test plan,
plan to get to early PDR, and program risk issues. Submit a candidate
Work Breakdown Structure (WBS) for SDD. This WBS shall also delineate
common versus system unique hardware and software components.
Provide
system/subsystem element analyses/data to support LSI/Govt risk assessment
analyses necessary to ensure that FCS embodies acceptable affordable
risk going into SDD.
Task
7
The integrator will provide support in the development of the
vehicle level specifications by the LSI for each of the vehicles in
table 1. The integrator will provide draft (legacy acceptable if
applicable to FCS) subsystem specifications, common and unique
for each of the vehicles.
Task
8
Define
armored chassis hull design definition capable of meeting or exceeding
the structural, ballistic, mine blast, & external attachment performance
and ICD requirements provided by the LSI within the platform weight
and dimensional requirements. Advanced lightweight performance and
synergistic solutions are encouraged. Support refinement to the subsystem
performance and interface requirements. Provide system attribute sensitivity
(i.e., weight, volume, threat capability, structural capability) to
potential growth in performance requirements as specified by the LSI.
Provide structural concepts for attachment of additional external
armor of other external items. The chassis hull is not limited to
a monocoque design.
Task
9
Provide
a fabrication concept that addresses building and assembling the chassis
hull components to performance requirements provided by the LSI and
in sufficient detail to support manufacturing plan development, including
tooling concepts, materials selections, quality assurance procedures,
and processing technologies. Provide structural concepts for attachment
of additional external armor of other external items. Provide preliminary
repair/maintenance concepts associated with structure/armor design.
Task
10
Provide
open architecture mobility subsystem hardware/software design definition
that supports block upgrades spiral development. The mobility subsystem
comprises the engine, energy storage, drive train, steering, suspension,
running gear and associated control and power electronics. Design
definition shall include functional schematics, simulation models,
and system metrics (weight, power, cooling, volume, RAM-D, etc.)
Task
11
Develop
a Vetronics system architecture for each variant which maximizes commonality
across the variant family of vehicles and defines the internal relationships
among Vetronics components as well as the relationships between the
Vetronics and the rest of the system and the C4ISR architecture.
Meeting
Support
Weekly
telecons to review schedule status, accomplishments, significant findings/conclusions/recommendations,
integration issues, etc.
Telecons
to start 1 wk after contract award and continue each week till contract
end. (Note: Not required the week of Initial and Final Coordination
Meeting)
Initial
Spec/ICD Development & Coordination Meeting - 11/19/02-11/20/02
Final
Spec/ICD Development & Coordination Meeting - 12/18/02-12/19/02
Schedule
Milestones
Subcontract
Start Date - 10/7/02
Subcontract
Completion Date - 12/20/02
Deliverables/
Data Requirements
(Note: Deliverables/Data to be provided in contractor format.) |
Delivery
Date (On dock at LSI)
|
- Issues/concerns
with initial system requirements, architecture and assumptions.
- Top
(potential) integration issues.
- Top
system risk areas
|
10/14/02 |
- Initial
report that includes status results from tasks 1, 2, 4, 6,
8, 9, 10, and 11.
- Draft
system specification inputs, subsystem specifications, and
ICD inputs, task 5 ,7
- CAD
models from task 3.
|
11/01/02 |
- Final
report that includes status results from tasks 1, 2, 4, 6,
8, 9, 10,and 11.
- System
specification, subsystem specifications, and ICD inputs, task
5, and 7.
- CAD
models from task 3.
|
12/06/02
|
Evaluation
Criteria
Supplier
proposal will be evaluated in each of the broad categories listed
below. Each category is allocated a maximum page count for consideration.
Each category must be addressed by the proposal. The sub-bullets are
intended to provide insight into the key areas of interest for each
category. Proposal submittals shall address these areas as well as
others that demonstrate significant category expertise that demonstrate
capability to execute the statement of work.
Technical
Approach (25-page (75,000-character) limit)
- Approach
to platform design commonality
- Approach
to developing concepts into preliminary design with evolving requirements
- Approach
to assess technology readiness for integration into platform design
- Approach
to spiral upgrade development and implementation
Understanding
of the Technical Challenges (5-page (15,000-character) limit)
- Identification
of top technology challenges
- Identification
of top integration challenges
- Identification
of top supportability challenges
- Plan
and processes for execution of the above statement of work.
Key Program
Challenge Mitigation Plans (5-page (15,000-character) limit)
- Mitigation
plan to address identified technology, integration, and supportability
challenges.
- Risk
management approach/process
- Weight
management approach/process