Tactical Missile Design Tactical Missile Design

422 Pages·2008·8.29 MB·English

PPrrooffeessssiioonnaall DDeevveellooppmmeenntt
SShhoorrtt CCoouurrssee oonn
TTaaccttiiccaall MMiissssiillee DDeessiiggnn
Eugene L. Fleeman
Tactical Missile Design
E-mail: [email protected]
Web Site: http://genefleeman.home.mindspring.com
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Introduction / Key Drivers in the Design Process
(cid:139)
Aerodynamic Considerations in Tactical Missile Design
(cid:139)
Propulsion Considerations in Tactical Missile Design
(cid:139)
Weight Considerations in Tactical Missile Design
(cid:139)
Flight Performance Considerations in Tactical Missile Design
(cid:139)
Measures of Merit and Launch Platform Integration
(cid:139)
Sizing Examples
(cid:139)
Development Process
(cid:139)
Summary and Lessons Learned
(cid:139)
References and Communication
(cid:139)
Appendices ( Homework Problems / Classroom Exercises,
(cid:139)
Example of Request for Proposal, Nomenclature, Acronyms,
Conversion Factors, Syllabus )
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Area Emphasis
Aero Configuration Sizing
Aero Stability & Control
Aero Flight Performance
Propulsion
Structure
Weight
Warhead
Miss Distance
Cost
Additional Measures of Merit
Launch Platform Integration
Primary Emphasis
Seeker, Sensors, and Electronics
Secondary Emphasis
Power Supply
Tertiary Emphasis
Safe, Arm, and Fuzing - Not Addressed -
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Comparison With
Tactical Missile Example of
Characteristics State-of-the-Art Fighter Aircraft
Axial Acceleration AGM-88
Maneuverability AA-11
Speed / altitude SM-3
Dynamic pressure PAC-3
Size Javelin
Weight FIM-92
Production cost GBU-31
Observables AGM-129
Range AGM-86
–
Kills per use Storm Shadow –
Target acquisition LOCAAS –
Superior Better Comparable – Inferior
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Propulsion Sizing /
Propellant or Fuel
Stabilizer
Diameter
Nose Fineness Geometry / Size
Wing Geometry / Size
Thrust
Profile
Flight Conditions ( α, M, h )
Length
Flight Control
Geometry / Size
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• Mission / Scenario Update
Definition
Initial Revised
• Weapon
Trades / Eval Effectiveness / Eval
Requirements,
Trade Studies
Initial Alt Baseline
and Sensitivity
Reqs Concepts Selected
Analysis
Initial Carriage /
• Launch Platform Iteration
Launch
Integration
Refine
Weapons
Req
• Weapon Concept
Alternate Concepts ⇒ Select Preferred Design ⇒Eval / Refine
Design Synthesis
• Technology
Initial Tech Initial Revised
Assessment and
Tech Trades Roadmap Roadmap
Dev Roadmap
Note: Typical conceptual design cycle is 3 to 9 months. House of Quality may be used to translate customer requirements
to engineering characteristics. DOE may be used to efficiently evaluate the broad range of design solutions.
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Define Mission Requirements
Alt Mission
Establish Baseline
Alt Baseline
Aerodynamics
Propulsion
Weight Resize / Alt Config / Subsystems / Tech
Trajectory
Meet
No
Performance?
Yes
No
Measures of Merit and Constraints
Yes
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(cid:139) Air-to-air Example SOTA 10 feet
• Short range ATA. AA-11. Maneuverability
• Medium range ATA. AIM-120. Performance / weight
• Long range ATA. Meteor. Range
Air-to-surface
(cid:139)
• Short range ATS. AGM-114. Versatility
• Medium range ATS. AGM-88. Speed
• Long range ATS. Storm Shadow. Modularity
Permission of Missile Index. Copyright 1997©Missile.Index All Rights Reserved
2/24/2008 ELF 8
EExxaammpplleess ooff SSuurrffaaccee--LLaauunncchheedd MMiissssiillee MMiissssiioonnss //
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Surface-to-surface Example SOTA 10 feet
(cid:139)
• Short range STS. Javelin. Size
• Medium range STS. MGM-140. Modularity
• Long range STS. BGM-109. Range
Surface-to-air
(cid:139)
• Short range STA. FIM-92. Weight
• Medium range STA. PAC-3. Accuracy
• Long range STA. SM-3. High altitude
Permission of Missile.Index. Copyright 1997©Missile.Index All Rights Reserved
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MMiissssiioonn RReeqquuiirreemmeennttss
Impact on Weapon Requirement
Aero Measures of Merit Other Measures of Merit Constraint
Aero Configuration Range / Time to Robust- Miss Observ- Launch
Sizing Parameter Weight Maneuver Target ness Lethality Distance ables Survivability Cost Platform
Nose Fineness
Diameter
Length
Wing Geometry / Size
Stabilizer Geometry / Size
Flight Control
Geometry / Size
Propellant / Fuel
Thrust Profile
Flight Conditions
( α, M, h )
Very Strong Strong Moderate – Relatively Low
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