High Energy Laser Weapons Systems Applications - The Black Vault

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SBL IFX DEMONSTRATION The SBL IFX is to include a cylindrical hydrogen fluoride, megawattclass laser with a 2.4- to 4.0-meter-diameter primary beam director and an integrated beam control system as depicted in Figure 7. Significant ground tests are planned to reduce SBL subsystem and integration risk through the accelerated development and integrated ground demonstration of first generation components: laser, beam control, beam director, and acquisition, tracking, and pointing subsystem. The IFX effort is to culminate in demonstration of the end-to-end capability to acquire, track, and destroy a boosting ballistic missile with a laser from space, as illustrated in Figure 8. Hydrogen-Fluoride (HF) Chemical Laser Spacecraft Bus (Attitude Control, Communications, & Power) Beam Expander (2.4m Monolith Mirror) Boost Phase Intercept Chemical Storage Beam Control (Pointing & Optical Quality) • Technology Demonstration of Boost Phase Intercept BMD from spa • Obtain performance data on integrated system performance • Demonstrate potential for space surveillance and space control mission • Built by a Joint Venture of Boeing, Lockheed Martin, and TRW Source: SBL Program Office Figure 7. Notional SBL Concept: Integrated Flight Experiment 14
Flight Vehicle Boosting Target Comm Relay Test Range Mission Control Center Figure 8. IFX Configuration Requirements Because the SBL IFX is a demonstration project, no formal mission needs statement (MNS) or ORD currently exists. However, Capstone Requirements Documents exist for Theater Missile Defense and National Missile Defense (NMD), both of which are applicable to SBL. In addition, requirements guidance for an SBL operational system appear in the Theater Missile Defense, National Missile Defense and Space Control MNS, and more specifically for IFX, in an SBL IFX Objectives Document signed in August 1999. SBL is to contribute to the mission need for “NMD engagement forces for boost-phase intercept, with adjunct mission application potential towards the needs of: • “TMD engagement forces at long stand-off range” • “neutralize enemy air defenses” • “improve precision of munitions delivery” • “improve range and reduce risks for target engagement” • “improve space surveillance responsiveness and effectiveness” • “improve theater fixed target ISR” • “provide offensive counter-space capability” • “provide defensive counter-space capability” 15
Page 1 and 2: Defense Science Board Task Force on
Page 7: TABLE OF CONTENTS EXECUTIVE SUMMARY
Page 11 and 12: INTRODUCTION Several decades of sci
Page 13 and 14: In addition, the task force was ask
Page 15 and 16: Findings: Current Initiatives Airbo
Page 17 and 18: Findings: New Applications Airborne
Page 19 and 20: Countermunitions Maritime Self- Def
Page 21 and 22: Findings: Science and Technology Th
Page 23 and 24: Include deployable optics technolog
Page 25 and 26: • Solid-State Lasers. Increase te
Page 27: CHAPTER I. CURRENT INITIATIVES
Page 30 and 31: • Lethality defines the total ene
Page 32 and 33: ABL PAC-3 FLOT THAAD Navy Theater W
Page 34 and 35: PATH TO OPERATIONAL SYSTEM Followin
Page 36 and 37: Technology Investment Schedule(FY)
Page 38 and 39: system, because loss resulting from
Page 42 and 43: Capability Assessment A definitive
Page 44 and 45: Top Risks for IFX Element ID Risk I
Page 46 and 47: Issue: No Operating System Concept
Page 48 and 49: • Beam Control (wavefront error a
Page 50 and 51: 00 01 02 03 04 05 06 07 08 09 10 HF
Page 52 and 53: The lower left part of Figure 17 sh
Page 54 and 55: 01 02 03 04 05 06 07 08 Relay Mirro
Page 56 and 57: 200 Funding ($M) 150 100 50 Tier 3
Page 58 and 59: HIGH ENERGY LASER SYSTEM - TACTICAL
Page 60 and 61: down of a single Katyusha rocket. I
Page 62 and 63: concentrations of .8% have been gro
Page 64 and 65: DF Lasers An artist’s conception
Page 66 and 67: TASK FORCE FINDINGS 1. The THEL ACT
Page 69 and 70: As technology matures, the operatio
Page 71 and 72: Space and Missile Defense Command a
Page 73 and 74: this pressure. Hence the ATL, using
Page 75 and 76: • They require a mirror constella
Page 77 and 78: optics a few KW would be required.
Page 79 and 80: fluids in order to improve output p
Page 81 and 82: This program will develop and demon
Page 83 and 84: mirrors be a significant part of th
Page 85 and 86: Cost ($B) $80 $60 $40 48 laser sats
Page 87 and 88: Space Ancillary Missions Ground Anc
Page 89 and 90: OBJECTIVES The objective of the EAG
Page 91 and 92:
2. Ground-, sea-, air-, and space-b
Page 93 and 94:
Air Force studies have identified p
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capabilities create a desired effec
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question of how weather and environ
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Figure 46. The Army Vision THE OBJE
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efore they could lock on and engage
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Current deuterium fluoride technolo
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elative near term, and support a po
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wavelength and CW and pulse wavefor
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COUNTERMUNITIONS The Army Space and
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• The Waste Heat Subsystem provid
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Figure 49. The Littoral Warfighting
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technology approach that has been u
Page 117 and 118:
Rules of engagement in operations o
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sight to the specific target(s). In
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Incorporating HEL systems into mili
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ADA integrator contractor to be imp
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triggered, need to be established u
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Maritime HEL Propagation 1 - 4.5 m
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In addition to the atmospheric phys
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A SOLUTION TO THE WEAPONEERING PUZZ
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Weapons Characteristics • Warhead
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REQUIRED WORK The Department of Def
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the extent that overall system leve
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BEAM CONTROL A recent study by the
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1st Generation 2nd Generation 3rd G
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• Many integration/demonstration
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Figure 67. Proposed Funding Profile
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concepts ranging from 50 to 300+ KW
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Free Volume = ~7 m 3 Beam Control S
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Table 3. Total SSHCL Weapon system
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8000 7000 Weight (kgs) 6000 5000 40
Page 159 and 160:
Although the patent for the laser w
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In the intermediate region, cost an
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ATMOSPHERIC PROPAGATION AND COMPENS
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econstitutes the laser fluids. A be
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Another concern for FELs, which hav
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Appropriately developed and applied
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• Tactical High Energy Laser - Fi
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APPENDICES
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A-1
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APPENDIX B. TASK FORCE MEMBERSHIP
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Dr. Ralph Schneider Mr. Mike Wardla
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October 19-20, 2001 Name Topic Col.
Page 189:
Capt. Jeff Barchers Dr. Al Ullman D
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TACTICAL HEL FIGHTER STUDY - BOEING
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• Enabling technologies critical
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In the future, the laser target eff
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Cloud Cover & Fog Molecular Absorpt
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P CFLOS = 0.8 Figure D-5. Notional
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egion on the right hand pie chart r
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• CUMULONIMBUS (CB) - Cauliflower
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With this brief discussion of the n
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In the future, off-board sensors wi
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Figures D-12 and D-13 illustrate po
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APPENDIX E. FREE ELECTRON LASERS
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straightforward with modest improve
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1. Develop ampere level average cur
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Spallation Neutron Source (SNS) thu
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RF Input Accelerator Optical Feedba
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picosecond electron pulses over tho
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APPENDIX F. GLOSSARY OF ACRONYMS AN
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GBL GGG GPS H 2 O 2 HE HE-HMMWV HEL
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