Precision Guided Mortar Munition (PGMM) XM395

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Precision Guided Mortar Munition (PGMM) XM395 1999 International Infantry & Small Arms Symposium 22 June 1999 Presented by: Greg Bischer AMSTA-AR-FSP-G

Briefing Purpose & Outline Purpose Information briefing Outline Program Focus Operational Considerations and Benefits Operation and Performance Summary

Program Focus AMC Description Maneuver task force commander s hip pocket precision indirect fire weapon Capability First round effects out to 12km (required) 15 km (desired) Target Set Focus Threats Within Protective Cover Bunkers Earth & Timber Concrete MOUT targets Buildings Fortified sniper positions Foxholes & Trenches Imperatives Low cost - Affordable (<$15K per round) No additional force structure Grenade Launchers (RPG- 7s), Crew Served Weapons, Command Posts, Observers, etc.

Warfighter Support Major General Carl F. Ernst CG USAIC Continuous & Significant User Support Requirement Document Approved EMD & Procurement Funding in POM Operational Experiments Continue Actively Support Technology Management Process STO, DTO, etc. MG Ernst articulates his vision for PGMM as the maneuver task force commander s hip pocket precision indirect fire weapon

Battlefield Payoffs AMC Reduced Collateral Damage Collateral Damage w/ today s best ammo w/ PGMM Capability Enables commander to engage enemy targets that are close to sensitive cultural areas Minimizes noncombatant casualties Lessons Learned From Chechnya US Personnel Casualties & Firing Time to Defeat Ammunition Requirements w/ today s best ammo w/ today s best ammo w/ PGMM Capability w/ PGMM Capability Improved Survivability & Accelerated Enemy Defeat Standoff kills Responsive kills One-shot kills Improved Deployability & Logistics Mortars are inherently deployable & tactically mobile. PGMM s accuracy will... Provide orders of magnitude increases in per round lethality Reduce size of logistics tail Russians struggled fighting in the city of Grozny. Close air support, attack helicopters, & armored vehicles did not fare well. Direct fire, close range methods of clearing buildings adversely affected survivability. Something like PGMM would allow them to send a bullet not a man while still minimizing collateral damage and noncombatant casualties.

PGMM Provides Leap-Ahead Lethality # of Rounds 450 450 400 400 350 350 300 300 250 250 200 200 150 150 100 100 50 50 0 Number of Rounds Required to Defeat Small, Protected Target vs. Range Current Round w/ MFCS Hundreds of Rounds PGMM w/ MFCS 1 Round 1 1 2 2 3 3 4 4 5 5 6 6 7 7 Range Problem gets worse if you are trying to defeat relatively small, protected targets. Practical limitations would preclude the use of current rounds against such targets Between 100 & 400 unguided rounds are required to defeat a small protected target. A precision guided mortar would enable defeat of a small, protected target with only one round.

Quantifying Combat Utility Recent series of warfighting experiments suggest... Reduced Collateral Damage Enabled engagements of targets close to culturally sensitive areas, non-combatants, or friendly troops Improved Lethality ~10x increase in indirect fire kills Improved Survivability ~50% improvement in blue force survivability Improved Deployability & Logistics ~40 % reduction in number of rounds fired Accelerated Enemy Defeat Significant reduction in time required to complete mission Quality time with users very valuable feedback Warfighting Experiments - M&S Primary Goal Continue to quantify the battlefield utility non-armor intensive type scenarios unique and valuable combined arms asset - significantly contributes to success of maneuver task force. Secondary Goal Obtain Operational Insights (DTLOMS Impact & TTP development) Support system design trade-off analyses (balance cost & performance) General Approach Constructive Simulations in JANUS & CASTFOREM Urban & Rural Terrain / Light & Heavy Infantry Near Term Sub-Experiments (JANUS) October 98 January 99 May 99 HR55 Vignette / Rural Heavy Rangers ARC JRTC MOUT ACTD August 99 HR49.x Vignette (Certified) Next Step Continue building vignette library Port JANUS HR4.9X runs to CASTFOREM early FY00

Growing Infrastructure Supporting PGMM MFCS: Digital Fire Control PGMM... An Integral Part of Modern Battalion Indirect Fire Commander s Interface Pointing Device Driver s Display Gunner s Display Fielded or WRAP Programs Observers Light-weight Laser Designator Range Finder (LLDR) Fire Control / C4I Links Mortar Fire Control System Linked to AFATDS / Embedded Battle Command 120mm Mortar Platforms M121 (carrier-mounted) M120 (towed mortar) Other encouraging signs Growing likelihood of adding 120mm mortar to the light forces Arms Room Concept 10th Mountain Division 75th Ranger US Marine Corps Turreted Mortar

Operation & Performance (Tech Demo Configuration) Altitude (m) 2500 2000 1500 1000 500 PGMM Flight Profile Apogee (for 12km down range distance) Glid e Destroy Target Acquire Target Flight Time (sec) 0.0 10 20 30 40 50 60 70 80 90 0.0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0 10.0 11.0 12.0 Down Range (km) Operational Sequence Drop fired Fins Deploy (<80ms) Wings Deploy at Apogee Glide for Extended Range Gyros sense in-flight location In-flight corrections made to guide to predetermined in-air basket (500m x 500m footprint on ground) Scans for laser designator energy on target Maneuvers to attack at optimum impact angle & at most vulnerable point. Performance Goals Accuracy: 1m Range: 0.5km - 15km Weight: <40 pounds Length: < 40 inches Unit Cost: <$15K

Major Subsystems (Tech Demo Configuration) Projectile / Guidance & Control Strapdown G&C Subsystem Low-Cost, Body-Mounted Gyros Fin Actuated Control System Post Launch Initialization Extended Range Glide Proportional Terminal Guidance GPS/INS Assembly (Under Investigation) 1 Seeker 2 Linear Position Measurement Sensor (Not a Quad) Hi-G Survivable Strapdown Real Time Processing / Code of the Day Warhead Optimized for threats behind protective cover Concept TBD Glide capability provides extended range without added cost, weight, & complexity of a rocket motor Theoretically superior design concept to gimbaled quad design Increased Reliability (No moving parts) 1. Tech demo will demonstrate GPS via simulation 2. Tech demo will demonstrate strapdown laser seeker via live fire demonstration

Airframe Based on German Bussard round Diehl Being modified to meet PGMM requirements Stepwise approach to qualification Fin Deployment Testing Wing Deployment/Ballistic Testing Range and Stability Experiment

Seeker Subsystem Sensor Section Gyro/ I/O & Mechanical Flight Processor Interface Section Features Inline optics (window, 2 lenses) Linear Position Measurement Sensor (Not a Quad) Strapdown (improved reliability and survivability Real Time Processing / Code of the Day Detector mounted directly onto electronics card to improve noise control Status Baseline design complete 3 different detectors being characterized (FEB - JUL 99) Noise Bandwidth Response / Detectivity Complexity (# of outputs) Cost Select Detector (SEP 99)

Gyro Subsystem Subsystem Components 3 Gyros (x,y, z) Flight Computer Clock Power Supply Gyro Vendor C.S. Draper Labs System can be easily upgraded to incorporate GPS Status Operated during wing deployment shock laboratory test Building units for subsystem High-G test (July 99) First operational flight test planned for Feb 00 (wing deployment flight testing) Subsystem Location Gyro ASIC

PGMM Guidance Study Purpose: Evaluate various guidance options to determine the payoff of accuracy versus cost for a potential EMD solution for PGMM. Guidance options being considered: Gyros only Full INS GPS* + Gyros GPS* + INS Analysis being done for 2 km, 4 km, 6 km, 8 km, 10 km, 12 km and 14 km flight ranges * GPS options will be studied with various levels of jamming resistance and recoverability.

PGMM Program Schedule FY95 FY96 FY97 FY98 FY99 FY00 FY01 FY02 FY03 FY04 FY05 FY06 FY07 FY08 FY09 Milestones ATD: Demonstrate technical maturity, combat utility, & affordability Range & Stability Demo Seeker Flight Demo Tech Base (ATD) MS I/II MS III EMD: Translate prototype design into a stable, producible, and cost effective system design EMD Prod.

Summary AMC Concept Description 120mm laser guided projectile with extended range glide capability Capability Responsive, precision, standoff defeat of bunker and MOUT targets Battlefield Payoffs Improved survivability Reduced collateral damage Accelerated enemy defeat Program Demonstrated technical progress and combat utility Continuing technical and operational experiments EMD Funding in POM with MS I/II decision in FY 01