1. GP45001017.ppt 42 nd Annual NDIA Targets, UAVs and Range Operations Symposium & Exhibition 17 November, 2004 Presented by:Ken Braucksick MA-31 Program Manager APPROVED FOR PUBLIC RELEASE

2.  Converted Russian Kh-31 Anti-ship missile (NATO AS-17 Krypton)  Currently Air launched from F-4  Launch Kit Implementation on F-16 in progress MA-31 Target Vehicle OVERVIEW  Typical Anti-ship missile profile: Mach 2.5 at 20 feet sea-skimming  Typical Anti Radiation Missile (ARM) profile Mach 3.5 at 48,000 feet APPROVED FOR PUBLIC RELEASE

3. GP45097002.ppt Approved for Public Release MIG-29M Su-27M Su-24M 9.Booster 10.Pneumatic Power Pack 11.Control Actuator 12.Ramjet Engine Sustainer MIG-27M 1.Passive Radar Homing Head 2.High Explosive Warhead 3.Automatic Unit 4.Power Pack 5.Battery 6.Autopilot 7.Fuel-Control Unit 8.Fuel Tank 1.Active Radar Homing Head 2.Radio Altimeter 3.Penetrating Warhead 1 2 45 6 7 8 9 10 11 12 3 1 2 3 Russian Kh-31 Supersonic Air- Surface Missile

4. Approved for Public Release 14.17 in. (360 mm) Dia 43.39 in. (1,102 mm) 30.67 In. (779 mm) Approx. Umbilical Connection Compartment-2 Access Door Booster Safety Lanyard Length Body Diameter Weight - Launch - Booster Burnout - Ramjet Ignition - Ramjet Fuel Depletion 185.0 in. (4,700 mm) 14.2 in. (360 mm) 1307 lb (593 kg) 1045 lb (474 kg) 952 lb (432 kg) 835 lb (379 kg) Control Fins (Titanium) Wire Tunnels - Phenolic Ejectable Inlet Covers Launch Lugs Nominal Airframe Characteristics 185.04 in. (4,700 mm) GP45097004.ppt MA-31 Air Vehicle

5. Nothing Else, Not in the US, France, or Wherever Has Demonstrated:  Sea Skimming at Mach 2.7  15G Multi-Axis Maneuvers While Sea Skimming  ARM Flight Profiles  High Altitude Cruise at Mach 3.5  Low Supersonic Signature  Threats A, B, & C Replication GP45011071.ppt 140 120 100 80 60 40 20 0 Altitude (1,000 ft) 012345 BQM-34S QF-4 MA-31 AQM-37C Steady Level Flight Airspeed (Mach Number) AQM-37C (EP) MQM-8G BQM-74E MQM-8G (ER/EER) SM-2 SSST APPROVED FOR PUBLIC RELEASE

6. 1996 – 2003 13 of 13 successful separations from F-4 (QF-4, F-4D) 3 of 13 post-launch failures 2 Russian power supply / fuel control 1 U.S. hardware - URAP F-4 Flight Test Operations APPROVED FOR PUBLIC RELEASE

7. GP45097011.ppt Typical Sea Skimming Profiles Delayed Boost Range (nm) 0 Time (sec) 0 15 92 24 110 31 152 Launch 33,000 ft, Mach 0.9 Sea Skim 5 m, Mach 2.5 Fuel Out Splash Booster Ignition 5000 ft Low Altitude Launch Range (nm) 0 Time (sec) 0 4 12 13 30 20 72 Launch 1,000 ft, Mach 0.8 Sea Skim 5 m, Mach 2.5 Fuel Out Splash Note: Actual customer profiles can be customized and multi-axis maneuvers may be added as desired up to 20g’s. APPROVED FOR PUBLIC RELEASE

8. Note: Actual customer profiles may vary. Typical ARM Profile Range (nm) 0 Time (sec) 0 27 60 36 77 46 110 Launch 33,000 ft, Mach 0.9 Fuel Out 43 94 DiveApogee 50,000 ft, Mach 3.5 APPROVED FOR PUBLIC RELEASE

9. Presentation Flexibility Precision Guidance  Universal Replacement Autopilot (URAP) derived from JDAM GCU (85K units delivered to date)  Provides improved endpoint accuracy –Self defense/close-in testing –Smaller safety corridor  Provides waypoint guidance –Precise control of flight path  Enables tracking of a moving endpoint –Maintains Position relative to shooter  Provides precise control of maneuver levels and onset rates – Max. threat replication!  Incorporates delayed boost ignition capability GP45011081.ppt Moving Aimpoint Receiver Antenna Moving Aimpoint/GPS Location Updates GPS Mobile Sea Target (MST) SDTS Post Boost GPS Acquisition Aimpoint GPS Receiver Antenna Aimpoint Moving GPS Location Transmitter Transmitter Antenna GPS Receiver Antenna HIT! APPROVED FOR PUBLIC RELEASE

10. Summary  MA-31 has already demonstrated: –Unparalleled performance / threat replication –The best reliability of any SSST in the last 4 decades –Exceptional presentation versatility –Exceptional cost effectiveness GP45011082.ppt MA-31 Represents THE Best Value for the USN APPROVED FOR PUBLIC RELEASE