1 / 10

GP45001017

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. GP45001017.ppt. MA-31 Target Vehicle OVERVIEW. Converted Russian Kh-31 Anti-ship missile (NATO AS-17 Krypton)

rsingh
Download Presentation

GP45001017

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


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

  2. MA-31 Target Vehicle OVERVIEW • 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 • 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. Russian Kh-31 Supersonic Air-Surface Missile 10 8 9 6 4 5 7 3 1 2 12 11 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 9. Booster 10. Pneumatic Power Pack 11. Control Actuator 12. Ramjet Engine Sustainer 2 1 3 1. Active Radar Homing Head 2. Radio Altimeter 3. Penetrating Warhead MIG-27M Su-24M Su-27M MIG-29M Approved for Public Release GP45097002.ppt

  4. MA-31 Air Vehicle 185.04 in. (4,700 mm) 43.39 in. (1,102 mm) 14.17 in. (360 mm) Dia 30.67 In. (779 mm) Approx. Booster Safety Lanyard Launch Lugs Umbilical Connection Control Fins(Titanium) Compartment-2 Access Door Nominal Airframe Characteristics 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) Ejectable Inlet Covers Wire Tunnels - Phenolic Approved for Public Release GP45097004.ppt

  5. 140 120 100 AQM-37C (EP) BQM-34S 80 Steady Level Flight Altitude (1,000 ft) BQM-74E AQM-37C 60 QF-4 MA-31 40 MQM-8G 20 MQM-8G (ER/EER) SM-2 SSST 0 0 1 2 3 4 5 Airspeed (Mach Number) 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 FlightProfiles • High AltitudeCruise atMach 3.5 • Low SupersonicSignature • Threats A, B, & C Replication APPROVED FOR PUBLIC RELEASE GP45011071.ppt

  6. F-4 Flight Test Operations 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 APPROVED FOR PUBLIC RELEASE

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

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

  9. NAVY Presentation FlexibilityPrecision Guidance GPS Post Boost GPS Acquisition GPS Receiver Antenna • 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 Moving Aimpoint Receiver Antenna Aimpoint GPS Receiver Antenna Aimpoint Moving GPS Location Transmitter Moving Aimpoint/GPS Location Updates Transmitter Antenna Mobile Sea Target (MST) SDTS HIT! APPROVED FOR PUBLIC RELEASE GP45011081.ppt

  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 MA-31 Represents THE Best Value for the USN APPROVED FOR PUBLIC RELEASE GP45011082.ppt

More Related