美军全球打击系统

Click to edit Master title style,Click to edit Master text styles,Second level,Third level,Fourth level,Fifth level,NDIA LRS Industry Team,10/5/2005,27,Click to edit Master title style,Click to edit Master text styles,Second level,Third level,Fourth level,Fifth level,*,Click to edit Master title style,Click to edit Master text styles,Second level,Third level,Fourth level,Fifth level,Click to edit Master title style,Click to edit Master text styles,Second level,Third level,Fourth level,Fifth level,NDIA LRS Industry Team,10/5/2005,8,Click to edit Master title style,Click to edit Master text styles,Second level,Third level,Fourth level,Fifth level,NDIA LRS Industry Team,8/30/2005,*,Draft,Draft,Draft,Draft,2005 NDIA/AAC Air Armament Symposium,Long Range Strike Industry Panel Brief,October 5, 2005,NDIA LRS Industry Team,Long Range Strike Industry Panel,LibertyWorks,TM,NDIA LRS Industry Team,Panel Membership,Alliant,Tech Systems,Robert Blake,Douglas Lewis,Gordon,Snurr,Aerojet,Mark Director,Pat Hewitt,Boeing,Carl Avila,Bob Marinan,Carl Miller,Steve Morrow,Ron,Mutzleburg,John Reilly,Glenn Vogel,Steve Vukelich,General Electric,Bill Dwyer,Honeywell,Dan Shockley,Liberty Works,John Arvin,Lockheed Martin,Barry Brown,Jim,Enault,Bob Hartmann,Richard Mitchell,Ed Whalen,Northrop Grumman,Gail Allen,Russ,Prechtl,Dave Rosenblatt,Orbital Sciences,Kevin Richardson,Pratt & Whitney,Richard,Kazmar,Raytheon,Dave Andrews,Louis,Galto,Robert Nelson,Charles Stevens,Rockwell Collins,Nick,Holoviak,Ken Kato,Williams International,Mike,Bak,Scott,Cruzen,Carl Schiller,Panel Chair: Carl Avila,Co-Chair :Ed Whalen,Co-Chair: Bob Nelson,Panel Advisors,Marya Bard:AAC/XR,Ed,Jackanowski,: ASN/RDA,NDIA LRS Industry Team,Long Range Strike Capability,SOF,Nuclear,C/B,Leadership,LRS,LRS,SOF,F/A-22 / F-35,Range,SOF,SOF,Enablers,Objective,Capability To Achieve Desired Effects Rapidly, Persistently, On Any Target, In any Environment, Anywhere, At Any Time,Requirements,Phase 1,:,Bomber Forces Upgrade:,Link -16 Connectivity, Stand Off, Precision, Radar, Targeting,Phase 2,:,Field Mid-Term Strike Capability:,Range, Persistence, L/O, Speed, GIG,Phase 3,:,Field Long Range Strike Capability,Long Range, Persistence, L/O, Speed, GIG, Transformational Technologies,USAF Next Generation Long Range Strike Study,NDIA LRS Industry Team,Potential missions/targets,:,TCS, Relocatable Targets, Fixed Targets, Counter-WMD, GWOT, HDBT, SUW, ,Global Strike Weapon,(High Speed Weapon),What it is,: A,Weapon,SYSTEM,NOT just a speed/propulsion,Potential launch platforms,:,TacAir, Surface Ships, Submarines, Bombers, ,Mach Number,6,“High Speed”,“Hypersonic”,2,It all depends on the,CAPABILITIES,Required,Milestone B,Target Set,Launch Platform,P,K,C4ISR,ConOps,Cost Analysis,TRL Assessment,JCIDS,JOINTNESS/Funding,AoA,10,Notional,Schedule,05,06,07,08,09,13,14,/,FY,AoA,JCIDS,MS B,RFP,SourceSel,IOC?,Studies,Sea Strike,Stealth / Standoff Platforms,Long Range (w/ tanking/support),Various POR/Cruise Weapons,Various conventional payloads,Medium Range: XXX - XXX+ nm,Speed: Mach X+,Warhead: XXX - XXX lbs,GW: XXXX lbs,“Platforms & Subsonic/LOE Weapons”,“JHS Strike Tactical Weapon”,Launch Platforms: B-2; F-117; Next-Gen High-Speed Bombers; CG/DDG; SSN; SSGN; TACAIR,Launch Platforms: TACAIR, SSGN, SSN, CG/DDG,Long Range:,3000 nm,Type: Conventional ICBM / IRBM,Large Warhead:,1000 lbs,GW: 3000 lbs,“Prompt Global Strike Weapons”,Launch Platforms: Silos, Heavy Bombers, SSGN,Fills Time Critical Warfighter Gap / Multi-Mission Capable,Allows Long Range Strike in Direct Attack Timelines,Notional TCS Capabilities Triad,C,4,ISR,WEAPONS,PLATFORMS,SENSOR TO SHOOTER DELAY TIME,UNIVERSAL ARMAMENT INTERFACE,DATALINK CONNECTIVITY,IT ALL DEPENDS ON:,THE,CAPABILITIES,REQUIRED,POTENTIAL MISSIONS/TARGETS,: TIME CRITICAL, RELOCATABLE, FIXED, COUNTER-WMD, GWOT, HDBT, SUW, - -,POTENTIAL LAUNCH PLATFORMS,: TACAIR, MARITIME PATROL, SURFACE SHIPS, SUBMARINES, BOMBERS, - -,CURRENT AND FUTURE CARRIAGE CONSTRAINTS,LRS and HSW are System of Systems,(Not Just a Range or Speed),TIME OF FLIGHT,NDIA LRS Industry Team,Warfighters Stand OffTime Critical Requirement,Kill Chain,Fix,Track,Target,Engage,Assess,Find,Major Investments Being Made in This Part Of The Kill Chain,Focus on Sensor to Shooter Delay Times of 10 Minutes or Less,We Focused on the “Weapons” Piece of the Kill Chain,NDIA LRS Industry Team,Time Critical Strike,Integrated Defense,Theatre Ballistic Missiles,Mobile/Moving Surface Targets.,Limited Deep GS Against HVT,CBRNE Defense,Maritime CAS,Fixed Targets,Close Air Support,Underground Facility,Customers Desired Capabilities,Time Critical Strike,Relocatable Targets,GWOT/High Value Targets,Counter-WMD,Surface Warfare (SUW),Fixed Targets,Naval Surface Fire Support,Hard/Buried Targets,USAF,USN,NDIA LRS Industry Team,Analysis Process,Derived System Characteristics,C4ISR & Targeting Performance,Target Set,Defensive Threat,Launch Platforms,Lethality,Block Speed,Accuracy,Survivability,Effectiveness,Compatibility,Probability of Survival,Reliability,Range,Capability Needs & Constraints,System Attributes or Key Performance Parameters,System Characteristics/TPM,Cost,Affordability,Payload Type/Size,Acquisition Cost,Technical Risk,Need Date,TRL,Reliability,NDIA LRS Industry Team,Concept 1,190” Length 2320 lbs Maximum Weight20.4” Diameter,Concept 2,250” Length 2320 -5500 lbs 20.4” Diameter,Vehicle Sizing,Platform and Configuration Constraints,Solid Rocket,Turbine,Pulse Detonation,Liquid Fuel Ramjet,Solid Fuel Ramjet,Variable Flow,Ducted Rocket,Dual Combustion,Ramjet,Scramjet,Propulsion,Subsystem,Candidates,Subsystem Constraints,Booster Required for Air Launch,(All Require Boosters For Surface Launch),LAUNCH PLATFORM,CANDIDATES,F/A-18 E/F,F/A-22 (EXTERNAL),JSF (EXTERNAL),F-16, F-15 E,B-2, B-52H, B-1,CG, DDG (MK-41/-75 VLS),SSGN/SSN,TACTICAL FIGHTER AIR LAUNCH (F/A-18 E/F, JSF, F-16, F/A-22, F-15E),194 IN. CONTAINER LENGTH FOR CV MAGAZINE ELEVATOR,1965 LB F/A-18 E/F ASYMMETRIC RECOVERY LIMIT,- POTENTIALLY 2320 LB,BOMBER, VLS/CLS (SSN, CG, DDG, SSGN),22 IN. BY 22 IN. MK-41 VLS CANISTER CROSS SECTION,250 IN. LENGTH OVER ALL (WITH BOOSTER) BOMBER,3300 LB MISSILE WEIGHT LIMIT (USING MK-41 VLS CANISTER),5000 LB FOR BOMBERS,LAUNCH PLATFORM SIZE CONSTRAINTS,TACTICAL FIGHTER AIR LAUNCH (F/A-18 E/F, JSF, F-16, F/A-22, F-15E),194 IN. CONTAINER LENGTH FOR CV MAGAZINE ELEVATOR,1965 LB F/A-18 E/F ASYMMETRIC RECOVERY LIMIT,- POTENTIALLY 2320 LB,BOMBER, VLS/CLS (SSN, CG, DDG, SSGN),22 IN. BY 22 IN. MK-41 VLS CANISTER CROSS SECTION,250 IN. LENGTH OVER ALL (WITH BOOSTER) BOMBER,3300 LB MISSILE WEIGHT LIMIT (USING MK-41 VLS CANISTER),5000 LB FOR BOMBERS,TACTICAL FIGHTER AIR LAUNCH (F/A-18 E/F, JSF, F-16, F/A-22, F-15E),194 IN. CONTAINER LENGTH FOR CV MAGAZINE ELEVATOR,1965 LB F/A-18 E/F ASYMMETRIC RECOVERY LIMIT,- POTENTIALLY 2320 LB,BOMBER, VLS/CLS (SSN, CG, DDG, SSGN),22 IN. BY 22 IN. MK-41 VLS CANISTER CROSS SECTION,250 IN. LENGTH OVER ALL (WITH BOOSTER) BOMBER,3300 LB MISSILE WEIGHT LIMIT (USING MK-41 VLS CANISTER),5000 LB FOR BOMBERS,NDIA LRS Industry Team,Target Set Considerations,Traditional fixed targets,Time Critical Targets,Mobile Targets,Moving Targets,WMD, Chem, Bio,HDBT,LRS And HSW Must Address Traditional, Time Critical and High Value Targets,Payload and Range Requirements for Different Target Sets Drive Vehicle Configurations,No single vehicle/ordnance pairing does it all,Delivery Vehicle Must Accommodate,Ordnance Blast Frag, Submunitions,Penetrator, CBRNE,Delivery accuracy,NDIA LRS Industry Team,Payload and Accuracy,Target Type,Payload HDBT MVR Hard Med Soft,250,500,750,1000,DE,SubMn,Cluster,Good,Moderate,Poor,Hard,Bunker, Shelter,Med,Runway, Bridge,Armor,Soft,Personnel, POL,HDBT,CBRNE, C2,SubMn,1000,750,500,250,CEP,SKR,LLDL,GPS,INS,HLDL,Todays Guidance Capability,Satisfies Accuracy Needs,Most Target Types At Risk With,Smaller Warhead,NDIA LRS Industry Team,Strike,Battlespace,Defined by Missile Range,vs,Time-of-Flight,200,600,1000,1400,1800,30,60,Range To Target (,nmi,),Time of Flight (min),Current Air/Surface Launch,Tactical Strike Capability,Mach 1,Mach 2,Mach 3,Mach 4,Mach 5,Mach 6,Mach 6,Mach 6,NDIA LRS Industry Team,Long Range High-Speed Missile Improves Time-Range,Battlespace,200,600,1000,1400,1800,30,60,Range To Target (,nmi,),Time of Flight (min),Art of the Possible Air/Surface Launch,Long-Range Strike Capability,Mach 1,Mach 2,Mach 3,Mach 4,Mach 5,Current Air/Surface Launch,Tactical Strike Capability,Mach 6,NDIA LRS Industry Team,High-Speed Missile System Range,vs,Time-of-Flight,Battlespace,200,600,1000,1400,1800,30,60,Range To Target (,nmi,),Near-Term,Technology,Fly out designed for fuel load, speed, and thermal,In-Service,Technology,Mach 1,Mach 2,Mach 3,Mach 4,Mach 5,Time of Flight (min),Mach 6,Mid-Term,Technology,NDIA LRS Industry Team,Low Risk Vehicle Design Points Provide Substantially Improved,Battlespace,200,600,1000,1400,1800,30,60,Range To Target (,nmi,),Near-Term,Air/Surface Launch 2320-5500 lb (Concept 2),Near-Term,Air/Surface Launch 2320 lb,(Concept 1),Mach 2,Mach 3,Mach 4,Mach 5,Time of Flight (min),Mach 6,NDIA LRS Industry Team,Warfighter Sensitivity to Speed,Initial Standoff Strike - Near-Peer Adversary Asset,Laydown,More Targets Reachable Before Hide Using High-speed Long-range Weapon,15,30,0,25,50,75,100,125,2,500 ft/sec,5,000 ft/sec,1,000 ft/sec,Capabilities-Based Analysis,Sensor-to-Shooter Delay (min),Normalized Targets,Engagable,WeaponBlock Speed,NDIA LRS Industry Team,Operations Research Models Long Range High-Speed Strike Weapons Benefits,Supersonic missile added to a baseline weapon set to,examine campaign level effect,Case 2,Baseline + HSW,vs,.,Stationary,TCTs,Range = 600,nm,Targets = Stationary,TCTs,Platform = Surface Launch,Case 3,Baseline + HSW,vs,.,Stationary,TCTs,Range = 600,nm,Platform = Surface,Launch+AIR,Case 1,Baseline,JDAM,JSOW A,JSOW B,Paveway,Maverick,JASSM,Tomahawk,ERGM,TCTs,: Time Critical Targets,HSW: High-Speed Weapon,Targets = Stationary,TCTs,NDIA LRS Industry Team,High-Speed Long-Range Capabilities Achieve Objectives Sooner,Air-launched Fast Weapons Showed The Most Benefit Due To High Sortie Rate,Benefit Achieved Is A Shorter Campaign,0,200,400,600,800,1,2,3,4,5,6,7,8,9,10,Days of Campaign,Cumulative TCT Kills,1. Current Weapons,2. High-Speed Weapon,(HSW),Stationary Target,Surface Platform,3. HSW, Stationary Targets,Air & Surface Platforms,NDIA LRS Industry Team,Survivability is Altitude, Speed and Observable Dependent,Speed,Altitude,Low P,S,Moderate P,S,Good P,S,Excellent P,S,High,Low,Low,High,Stealth Driven Improvement,NDIA LRS Industry Team,Operational Availability,Long Range Strike Weapons Will Be Highly Reliable,Reliability Designed In and Verified in Development,Wooden Round,Reliability As a Key Performance Parameter,Minimum Support Infrastructure,NDIA LRS Industry Team,Technology Readiness Level (TRL) Flight Vehicle Subsystems Focus,System Integration,Airframe,- Structure,- Control Surfaces,- Thermal protection,Guidance, Navigation, and Control,- Guidance and Control Unit IMU ,Data Link,- Actuators,- Seeker/,Radome,/IR Dome as required,Payload,-,Penetrator/,Blast,Frag,/,Thermobaric,/,Fuzing,/,Submunitions,/,Advanced Payloads,Propulsion,- Inlet/Flow Path,- Fuel Liquid/Solid,- Combustor/Turbine/Fuel Control,BLUE: Design/Development Materials/Processes Readily Available Across Industry,GREEN: Focus Investment to Attain TRL 6/7; Target Set/Mach Number Dependent,Generic Vehicle Architecture,NDIA LRS Industry Team,Concept,05,06,07,08,09,10,11,12,13,14,15,16,17,18,Solid Rocket,9,9,9,9,9,9,9,9,9,9,9,9,9,9,Supersonic Turbojet,6,6,6,7,7,7,7,7,7,7,7,7,7,7,Liquid Fueled Ramjet,9,9,9,9,9,9,9,9,9,9,9,9,9,9,Variable Flow Ducted Rocket,8,9,9,9,9,9,9,9,9,9,9,9,9,9,Dual Combustion Ramjet,6,6,7,7,7,7,7,7,7,7,7,7,7,7,Solid Fueled Ramjet,5,5,5,6,6,6,6,6,6,6,6,6,6,6,SCRAMJET,6,6,6,6,7,7,7,7,7,7,7,7,7,7,Pulse Detonation Engine,4,4,4,5,6,6,7,7,7,7,7,7,7,7,Propulsion Technology Readiness Levels,HyFly Flight Demo Program (M=4-6),Fiscal Year,VAATE Ground Testing (M=4+),NASA Wind Tunnel Tests,GQM-163A Flights (M=2.5); In Production,MA-31 Operational Use (M=2.5-3.5),Many Examples of Operational Solid Rockets,RATTLRS Flight Testing (M=3-4),SED Flight Tests (M=4.5-6.5),LRS/HSW,Considerations,Low ISP, Sizing Not Suitable,RATTLRS/VAATE Adding Maturity,Mature, in Production,Mature, in Production,HyFly Adding Maturity,Funding Limited Schedule to Mature,No Govt. Funded Plans to Mature,No Govt. Funded Plans to Mature,Propulsion Technology Supports FY-08 Program Start,NDIA LRS Industry Team,Vehicle Concepts,SCRAMJET,Dual Combustion RAMJET,Variable Flow Ducted Rocket,Supersonic Turbo Jet,Liquid Fuel RAMJET,NDIA LRS Industry Team,Notional,Acquisition,Program,Constant Base Year 2005 Dollars,SDD Period of Performance : Oct 2007 thru Sept 2012,50 Equivalent Test Units Delivered,Production Quantity Assumed to be 4,000 Units,Excludes Pre-SDD Concept / Technology Development Cost,Assumes All Up Round no GFE Required for Production,Excludes Government Program Office, Test Facility, and Support Costs,Integration on one USAF and One USN platform,2005,2006,MS B,MS A,MS C,Ongoing Risk Reduction,2007,2008,2009,2010,2011,2012,2013,2014,2015,2016,2017,System Design & Development,DT / OT,IOC,SDD Program = $800-900 M AUPP= $500-800 K,Full Production,Low Rate Production,NDIA LRS Industry Team,Summary and Recommendations,High Speed, Long Range Weapons Have The Potential To Be A Significant Force Multiplier,Technology Readiness of Critical Subsystems Supports FY-08 Program Start,USAF and USN Studies are Addressing the Same Requirement,Development Cost Consistent with Current Generation Weapons,Strong, Competitive Industrial Base,Establish Joint Requirements (JCIDS),Coordinate Government Planned,AoAs,in FY-06 (USAF & USN),Conduct Program Cost Estimates to Support FY-08 POM,Recommendations,Summary,NDIA LRS Industry Team,