APKWS II Turning 2.75-Inch Rockets into Precision Guided Munitions 15 May 2012
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1 APKWS II Turning 2.75-Inch Rockets into Precision Guided Munitions 15 May 2012 Chuck Paras Atkinson Aerospace and Technology Engineering Support PMA-242 Direct and Time Sensitive Strike Program
2 2 Advanced Precision Kill Weapon System II (APKWS II) APKWS is highly effective weapon that allows aviators to complete their missions while minimizing the risk of harm to allies and non-combatants.
3 3 Advanced Precision Kill Weapon System II (APKWS II) APKWS is a Semi-Active Laser (SAL) guidance kit added to current 2.75-inch Rockets Manufactured by BAE Systems Low collateral damage and minimal aircraft integration Accurate: <1 meter CEP in Test Program Increased Kills/Sortie: up to 76 per sortie Status: Jan 2012 Feb 2012 Mar Completed Operational Testing Fielding Decision by USMC Initial Operational Capability Full Rate Production Decision 2012 High Precision, Low Collateral Damage Weapon Deployed
4 4 APKWS II Weapons System Overview Program of Record LAUNCH PLATFORM Joint Capabilities Tech Demo Legacy Launchers USN/USMC - LAU-61/LAU-68 LASER SOURCE Legacy Launchers USN/USMC - LAU-61/LAU-68 USAF - LAU-131 USA - M260/M261 APKWS II NTS GLD FLIR
5 5 APKWS II System Aiming Cues UH-1Y SCS 7 Fuze Shipping and Storage Container, CNU-711/E (4 WGU-59/B) Guidance System, WGU-59/B Warhead MK 66 Mod 4 Rocket Motor Fastpack PA-150 (4 AUR) Mk 152 HE w/ Mk435 Mod 0 fuze M151 HE w/ M423 fuze AUR Length/Weight: 73.8-inches /32.8 lbs 7-Tube LAU-68 F/A Launcher AH-1W, UH-1Y APKWS HE Impact
6 6 APKWS Comparison WGU-59/B APKWS II 2.75-Inch Rocket Length 73.8 inches MK 435 Fuze Unguided 2.75 Inch Rocket Length 55.3 inches Weight Diameter Longitudinal CG Lateral CG 32 lbs Weight 23 lbs MK inches inches (max HE Diameter inches (max bourrelet) bourrelet) inches Longitudinal CG inches inches APKWS II Guidance Section Lateral CG inches LAU-68 F/A Launcher Features Unguided 2.75-inch APKWS II LAU-68 D/A or LAU-61 C/A Launcher MK-66 Mod 4 RM M151/MK152 WH Point Detonating Fuze MK 66 Rocket Motor LAU-61/LAU-68 Launcher PA-92 Shipping & Storage Container SAL Guidance Section CNU-711/C Shipping and Storage Container
7 7 APKWS How it Works 1. DASALS TM Seeker optics receive laser energy from target 2. Seeker electronics convert laser intensity to determine target angle 3. IMU (Atlantic Inertial Systems) senses rocket pitch, yaw & roll 4. Autopilot uses IMU data and seeker data to calculate flaperon positions, which are sent to the Control Actuation System (CAS) 5. CAS moves flaperons to commanded locations and airframe reacts to hit target DASALS TM is a trademark of BAE Systems, Inc
8 APKWS Off Axis Capability 5000 meter shot 3000 meter shot Thousands Surface Danger Zone -1,600 to 12,750 meters (longitudinal) ±8,000 meters (lateral) 1400 meter shot 2m Average Miss Distance: 0.44 meters NDIA APKWS BRIEF V4 8
9 9 Concept of Operations APKWS II
10 10 Fixed Wing APKWS JCTD Shots & Military Utility Assessment Spring 2013 Unchanged for FW APKWS II Guidance: Control Actuation system Modification Environmental: Wing Slot Seal Modification Wing Deployment: Wing Slot Seal Cracker Wing Deployment Updated for FW APKWS II
11 APKWS II Program of Record Qualification Testing Complete Laboratory/Ground Tests Summary Environmental Qualification Adjacent Rocket Fire Hazards of Electromagnetic Radiation to Ordnance Drop Tests Handling (37 ) & Safety (40 ) Shipboard Shock Electromagnetic Environmental Effects (E 3 ) Ground Launch at Targets from 1.5 to 5 Km First Article and Lot Acceptance Tests Flight Tests Captive Carriage & Safe Separation Integrated Flight Tests (IT-B and IT-C) Operational Assessment (OT-B) Initial Operational Test and Evaluation (IOT&E) NDIA APKWS BRIEF V4 11
12 Production Low Rate Initial Production Lot 1 Delivered Lot 2 in Manufacture Full Rate Production In Negotiation NDIA APKWS BRIEF V4 12
13 13 Other Applications Same interface as unguided rockets Simple qualification for follow-on platforms MQ-8B Firescout Rapid Deployment Capability AT-6 Texan F- 18 Hornet Follows Fixed Wing JCTD Industry Funded Demonstration
14 14 Summary APKWS II in production Units being tested in combat Success in combat will inform future plans Questions?
15 15 Contact Info Charles Paras Rockets System Engineer PMA-242-Direct and Time Sensitive Strike Program
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