News HAVE STAR

National Air Intelligence Center

Acquisition Integration Division

Wright-Patterson AFB OH 45433-5637

TASK ASSIGNMENT GUIDE (TAG)

Date: No:

1. (U) TITLE: Land Attack Cruise Missile Engineering Design - Level 2

2. (U) THREAT AREAS: 3.2 Threat Targets

3. (U) STATEMENT OF NEED: This task will provide a Level 2 engineering design of a Land Attack Cruise Missile (LACM) system. This effort will include designs of all subsystems, including all warhead options, and will use the most current information available from NAIC.

This task will be divided into two subtasks as follows:

a) Provide a Level 2 engineering design of the a specific Land Attack Cruise Missile system as directed by NAIC. Characteristics that will be reported as part of the Level 2 design will include, but will not necessarily be limited to, those listed in Atch 1.

b) Provide in writing an uncertainty analysis documenting the design trade-offs and design choices made in Subtask a. Included are choices in materials, structural designs, subsystem designs, and electronic components. The uncertainty analysis for the design will include, but not necessarily be limited to, probability of occurrence and rationale for choices using the Estimating Qualifiers and Design Selection Rationale shown in Atch 2.

4. (U) PERIOD OF PERFORMANCE:

5. (U) REPORTS REQUIRED: For obtaining coordination and approvals, five draft copies of the final report will be required. Reporting will be IAW the CDRLs and DoD-0000-151C-95. For the final report, two camera-ready copies plus one copy of magnetic media are required for both word processing and graphics files. These should be in Microsoft WORD file format. Any non-computer graphics for this task will be provided in separate form, without captions, from the final documentation.

Y2K Compliance Checklist Required? ________(yes) __________(no) (Check One)

6. (U) DESIRED DELIVERY DATE FOR TIP: 30 days from receipt of TAG.

7. (U) ESTIMATED COST:

8. (U) TAG MONITOR/OFFICE: Mr. John Tuss, NAIC/GTA

9. (U) TECHNICAL MONITOR:

10. (U) COORDINATION:

TAG MONITOR ________________________________ DATE __________

TECHNICAL MONITOR _____________________________ DATE __________

DIVISION CHIEF________________________________ DATE __________

FAE/COR ______________________________________ DATE __________

CONTRACTING OFFICER _________________________ DATE __________

 

ATTACHMENT 1

CHARACTERISTICS REQUIREMENTS

General1. Design information of sufficient detail for use with full, six degree of freedom flight simulation computer programs.

2. Design load requirements and safety factors.3. Dimensional tolerances for all major components.4. Alternate materials for all major components.5. Mission and performance specifications.

6. Position update system description.

7. Mass and balance.8. Flight controls (types, locations, dimensions, materials, component types).

Airframe 1. Locations, dimensions, and masses of all major subsystems.

2. Airframe structural design, dimensions, and materials.

3. Fuel tank dimensions and materials.

4. Tank operating pressure as a function of time.

5. Tank burst pressure.

6. Fuel type.

7. Flight load limitations.

8. Locations and dimensions of overwraps, liners, or Radar Absorbing Materials (RAM), if used.

 

Propulsion

1. Engine location, external dimensions and materials.

2. Internal component layout, dimensions, and materials.

3. Thrust performance capability.

4. Fuel consumption performance capability.

 

Avionics/Guidance system

1. Primary component locations and external dimensions.

2. Battery and power supply location, dimensions, materials, component types.

3. Auxiliary/supporting electronics locations, dimensions, materials, component types.

4. Component technology types or levels.

5. Definition of any transmitted and/or received RF and EO signals.

6. Accuracy.

 

Warheads

1. Type, location, external dimensions and materials.

2. Deployment mechanism.

3. Internal layout, dimensions and materials.

4. Fuse location, dimensions, materials, and component types.

5. Auxiliary/supporting electronics locations, dimensions, materials, component types.

6. Environmental control system type and location.

7. Type, location, external dimensions of any pyrotechnic devices.

 

 

 

Countermeasures

1. Type, location, external dimensions, and materials.2. Deployment mechanism.3. Internal layout, dimensions and materials.4. Battery and power supply location, dimensions, materials, component types.

5. Auxiliary/supporting electronics locations, dimensions, materials, component types.

6. Component technology types or levels.

7. Definition of any transmitted and/or received RF and EO signals.

 

ATTACHMENT 2

ESTIMATING QUALIFIERS

CODE

DESCRIPTOR

PROBABILITY (%)

RELATED TERMINOLOGY

P1

Near Certainty

90 - 99 Percent

Will, shall, is expected, is anticipated, highly likely, highly probable, virtually (almost) certain

P2

Probable

60 - 90 Percent

Likely, we believe, we estimate, chances are good

P3

Even Chance

40 - 60 Percent

Fifty-fifty, medium probability

P4

Improbable

10 - 40 Percent

Unlikely, low probability, probably not, we believe...not

P5

Slight Chance

1 - 10 Percent

Highly doubtful, near impossible, almost impossible, very low probability

0

No chance

0 Percent

Impossible, could not occur, absolutely not

 

DESIGN SELECTION RATIONALE

CODE

CATEGORY

DEFINITION

R1

Intelligence

Estimate based on published intelligence products, available intelligence data, intelligence community direction or preference.

R2

Known Design Practice

Estimate of designer's choice based on options described in textbooks, handbooks, journals, and other publications of the producing entity.

R3

Task Guideline or Ground rule

Characteristic or constraint specified in definition of the task scope.

R4

Engineering Judgment

Engineering estimate based on evaluation of factors such as application of physical principles, manufacturing practice or constraints, reliability estimates, design risk, life cycle cost considerations, access or availability for routine maintenance.

R5

Functional Need

Design characteristics inherent to the operation of a subsystem or component.

R6

Mirror Image

Estimate based solely on US technology or design practice.