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F-35_武器系统

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F-35_武器系统 © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -1 Public Release JSF 10-205 4/14/10 F-35 Weapon System Overview DISTRIBUTION STATEMENT A: Approved for public release; distributi...
F-35_武器系统
© 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -1 Public Release JSF 10-205 4/14/10 F-35 Weapon System Overview DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited Doug Hayward Deputy Director F-35 Vehicle Systems Lockheed Martin Aeronautics © 2010 Lockheed Martin Aeronautics Company © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -2 Public Release JSF 10-205 4/14/10 3 Services 8 International Partners 2 Security Cooperation Participants P&W F135 GE/RR F136 Team JSF Autonomic Logistics Integrated Training 3 Flight Test Facilities Global Sustainment Interoperability CTOL CV STOVL Domestic / International Suppliers JSF SDD Program Overview CATB © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -3 Public Release JSF 10-205 4/14/10 Lethal Survivable Supportable Affordable • Stealthy, Supersonic, Multirole, STOVL • Joint and Coalition Interoperability • F-16 / F/A-18 Speeds and Performance • Advanced Avionics and Data Links • Advanced Countermeasures • Increased Endurance / Range With Internal Fuel and Weapons • Smaller Logistic Footprint…Requiring Less Support and Airlift F-35 5th Gen Multi-Role Fighter © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -4 Public Release JSF 10-205 4/14/10 Weapons Carried Internally Low-Emission Radar and Avionics Low Observable Seams, RAM Seals Curved Diverterless Inlets, “Buried” Engine Antennas Embedded / Internal Antennas and Sensors DAS Apertures EOTS / IRST Reduced Signature Nozzle Aircraft Shaping and Edge Alignment Fundamental 5TH Gen Design Features Can Not Be Retrofitted Large Capacity Internal Fuel Tanks VLO Stealth Must Be Designed-In CTOL 18,500 lbs STOVL 14,000 lbs CV 20,000 lbs © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -5 Public Release JSF 10-205 4/14/10 Multi-Mode Sensors Precision Weapons Energy Maneuverability Net-Enabled Ops Integrated Sensor Fusion Advanced Stealth With Fighter Performance 5th Generation Fighters (Circa 2005 ) 4th Generation Fighters (Circa 1975 )C ap ab ili ty Time F-35 Is the Future The Solution – A Quantum Leap In Capability © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -6 Public Release JSF 10-205 4/14/10 Lockheed Martin Multi-Service Design Short Take-Off and Vertical Landing (STOVL) Carrier Variant (CV) Conventional Take-Off and Landing (CTOL) Lift Fan Roll Posts 3-Bearing Swivel Nozzle Strengthened Landing Gear and Tailhook Wingfold and Ailerons Added Larger Wing and Horizontal Tail Area Internal 25mm 4-Barrel Gattling Gun In-Flight Refueling Door (Boom) Probe and Drogue Refueling (Basket) Probe and Drogue Refueling (Basket) Centerline Gun Pod with 25mm Gun © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -7 Public Release JSF 10-205 4/14/10 CTOL Comparison (USAF) F-35 CTOLF-16 F-22 Length 49.7 ft Span 31 ft Wing Area 300.2 ft2 Internal Fuel 7,162 lb Length 51.4 ft Span 35 ft Wing Area 460 ft2 Internal Fuel 18,483 lb Length 62.1 ft Span 44.5 ft Wing Area 840 ft2 Internal Fuel 18,448 lb © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -8 Public Release JSF 10-205 4/14/10 Air-to-Surface Electronic Attack • Very Low Observable Stealth • Fighter Performance • Integrated Sensor Fusion • Net-Enabled Operations • Peace Keeping Capabilities • Advanced Sustainment Air-to-Air Command &Control Carrier Short Takeoff F-35 Redefines Multi-Role Aircraft ConventionalIntelligence, Surveillance, Reconnaissance Multi-Mission Capability © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -9 Public Release JSF 10-205 4/14/10 Day Night Data Links / Interrogators / EW Suite … Multi-Spectral Sensors Fused Tactical Information Managed & Displayed To The Pilot Ground Moving Target Missile WarningElectro-OpticalRadar Total Situational Awareness © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -10 Public Release JSF 10-205 4/14/10 A Quantum Leap in Capability Unprecedented Effectiveness...and Value R el at iv e Lo ss Ex ch an ge R at io Legacy 1 >6 F-35 Air-to-Air Better R el at iv e Ac qu is iti on C os t Legacy 1 1 F-35 Acquisition Cost Better Legacy 1 0.8 N or m al iz ed O & S C os t F-35 O&S Cost Better Legacy 1 >6 R el at iv e D et ec tio ns & ID F-35 ISR Better Legacy R el at iv e K ill s F-35 1 Air-to-Ground 8 Better © 2009 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Nov 09-11 Public Release F-35 Weapon Carriage Overview “Putting the Strike in the Lightning II” © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -12 Public Release JSF 10-205 4/14/10 CTOL Internal Gun Store Fully Certified During SDD Stormshadow GBU-16 Paveway II 1,000-lb LGB (MK-83 Warhead) AIM-9X Sidewinder MK-84 BSU-50 Ballute 2,000-lb HDGP GBU-24A/B Paveway III 2,000-lb LGB (MK-84 / BLU-109 Warhead) CBU-99/100 Rockeye II Cluster Munition 426 -Gallon Wing Tank GBU-10 Paveway II 2,000-lb LGB (MK-84 Warhead) MXU-648/CNU-88 Baggage Pod BDU-57/58/60 Laser-Guided Training Round AGM-158 JASSM EXTERNAL WEAPONS EXTERNAL WEAPONSINTERNAL MK-82 500-lb LD & HD GBU-12 Paveway II 500-lb LGB (MK-82 Warhead) AIM-120B/C AMRAAM AIM-120C AMRAAM Brimstone/Joint Common Missile GBU-12 Paveway II 500-lb LGB (MK-82 Warhead) GBU-31 JDAM 2,000-lb (MK-84 Warhead) AGM-154A/C JSOW Glide Bomb GBU-31 JDAM 2,000-lb (BLU-109 Warhead) AIM-132 ASRAAM Brimstone/Joint Common Missile GBU-32 JDAM 1,000-lb (MK-83/BLU-110 Warhead) Missionized Gun UK 500# PGB Phase I SDB GBU-38 JDAM 500-lb (MK-82 Warhead) MK-83 BSU-85 HDGP MK-84 2,000-lb LD/HDGP MK-83 BLU-110 LDGP 1,000-lb LDGP Weapons Currently Under Development AGM-154A/C JSOW Glide Bomb GBU-31 JDAM 2,000-lb (MK-84 Warhead) MK-76/MK-58/BDU-48 GBU-32 JDAM 1,000-lb (MK-83/BLU-110 Warhead) GBU-31 JDAM 2,000-lb (BLU-109 Warhead) AIM-132 ASRAAM GBU-38 JDAM 500-lb (MK-82 Warhead) Weapons Carriage Requirements © 2009 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Nov 09-12 Public Release © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -13 Public Release JSF 10-205 4/14/10 SMS Hardware I/O Structure (No OFP) - Provides Legacy Non-1760 Interface - Provides Growth Flexibility for Future Stores MIL-STD-1760C Class 1 Interface at A/G Stations - Tailored Class 1 at A-A - 8 Independent ‘1553 Channels GAU-22/A 25mm Gun - Internal (CTOL) - Missionized (STOVL/CV) 6 External Hardpoints Fwd of MLG - Air-to-Air and Air-to-Ground Pylons - Advanced Rail Launchers and AME Internal Weapon Bays - Combined A-G and A-A - 2000 lb on CTOL & CV - 1000 lb on STOVL - Internal Adapters Non-Pyrotechnic S&RES - Improved Supportability Centerline Station On All Versions - Structural & Tailored (STOVL) Mil-STD-1760 Class 1 - Missionized Gun (STOVL & CV) Single Point Safing From Outside Cockpit Weapon Integration Overview Weapon Supplier and Data Management Stores Management Systems Armament Carriage Systems Stores Certification Process Management Weapon Bay Integration © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -14 Public Release JSF 10-205 4/14/10 F-35 Weapons Stations 11Station 10 9 3 2 1 A/AStore A/A, A/S A/A, A/S A/A, A/S A/A, A/S A/A 300Capacity CTOL/CV 2,500 5,000 6 Gun 1,000 8 A/A, A/S 2,500 7 A/A 350 5 A/A 350 4 A/A, A/S 2,500 5,000 2,500 300 Capacity STOVL 300 1,500 5,000 1,0001,500 350 350 1,500 5,000 1,500 300 Over 18K lbs Of Payload Capability © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -15 Public Release JSF 10-205 4/14/10 Weapon Bay Stay-Out Volumes Definition • Weapon Stay-Out Volumes Defined to Protect Internal Bay Volume • Includes All Required Weapons Plus Static, Fall and Maintainer Access Clearances • Incorporates Internal Bay Design Lessons Learned • Additional Clearance for Access and Flow- Field Effects © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -16 Public Release JSF 10-205 4/14/10 Weapon Loading Validation Ship – Air Integration Lab Utilized To Substantiate Loading Prior to First Load Real Time Motion Capture Real-Time Immersive Simulation Aircraft Load © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -17 Public Release JSF 10-205 4/14/10 F-35 Gun System Development • General Dynamics GAU-22/A Gun System • 3,000 SPM Four Barrel Derivative of GAU-12 • Currently Qualified with PGU-20/U API and PGU-23 TP Ammunition • Primary Mission A/G with A/A Fallout Capability • Internal Installation for CTOL • 181 Rounds Linear Linkless Feed System • Over 50,000 Rounds Fired in Development and Qualification • Qualification Completed in 2008 • Missionized Pod for STOVL and CV • 220 Rounds Helical Feed System • Currently in 36,000 Round Qualification Test Program © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -19 Public Release JSF 10-205 4/14/10 Block 0.1 – First Flight and Envelope Expansion Basic functions to get the Aircraft Flying Block 0.5 – Initial MS Architecture & Sensor Infrastructure Mission systems infrastructure Build supporting sensor and architecture development Block 3 – Enhanced Warfighting Follow-on build to incorporate advanced decision aids, threshold weapons, and limited objective functionality Block 1 – Initial Warfighting Capability Support for the AI mission (limited target set) allowing meaningful operational test Block 2 – Multi-Mission Support Added support for CAS with expanded target set (sensor detection and weapon prosecution) Supports 7 Flight Performance Aircraft Initial MS Tactical Sensors Integration “Avionics FF(A3)” Initial Weapons Testing Bulk of MS Hardware on Board Primarily Software Updates with Added Weapons JSF Capability Upgrades Through Spiral Block Plan © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -20 Public Release JSF 10-205 4/14/10 F-35 - Designed for Future Weapon Growth • Internal Weapon Bay Design Provides Physical Volume for Future Weapons • Future Weapon Designs Should Use F-35 as Design Driver! • External Station Spacing and Capacity Sized for Larger External Stores • All S&RE and AME Designed for MIL-STD-8591 Mechanical Interfaces • MIL-STD-1760 Class 1 Interface Provided at All Store Stations • Modular Software Architecture to Minimize Integration Impacts © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -21 Public Release JSF 10-205 4/14/10 Program Schedule CY 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 FY 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 2017 System Development and Demonstration Developmental Operational Low-Rate Initial Production & Multiyear Procurement 2018 20182017 USMC USAF USN EOQ CV CTOL AA-1 STOVL Multiyear 1 Initial Operational CapabilityFirst Flights Test Completions CATB BF-1 LRIP 1 (2) LRIP 2 (12) LRIP 4 (32) LRIP 3 (17) Planned Production • Air Force 1,763 CTOL • Dept of Navy 680 CV/STOVL • Partners 800-1500 LL JESB Profile F-35 Program Information AF-1 LRIP 5 (52) LRIP 6 LRIP 7 LRIP 8 © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -22 Public Release JSF 10-205 4/14/10 LRIP Aircraft Now on Moving Line The Moving Line © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -23 Public Release JSF 10-205 4/14/10 BF-3 During Structural Coupling Test - Aug. 13 – 17, 2009 © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10-23 Public Release In Ground Testing © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -24 Public Release JSF 10-205 4/14/10 In Flight Testing © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -25 Public Release JSF 10-205 4/14/10 © 2010 Lockheed Martin Aeronautics Company DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Mar 10 -26 Public Release JSF 10-205 4/14/10 In Flight Testing STOVL at USN Test Facility Slide Number 1 JSF SDD Program Overview F-35 5th Gen Multi-Role Fighter VLO Stealth Must Be Designed-In The Solution – A Quantum Leap In Capability Lockheed Martin Multi-Service Design CTOL Comparison (USAF) Multi-Mission Capability Total Situational Awareness Slide Number 10 Slide Number 11 Weapons Carriage Requirements Slide Number 13 F-35 Weapons Stations Weapon Bay Stay-Out Volumes Definition Weapon Loading Validation F-35 Gun System Development JSF Capability Upgrades Through Spiral Block Plan Slide Number 20 Program Schedule The Moving Line Slide Number 23 Slide Number 24 Slide Number 25 Slide Number 26
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