OBJECTIVES:

• PROVIDE S&T BASE TO SUPPORT RAPID STRIKE (RE)PLANNING AND EXECUTION FOR CRUISE MISSILE AND TACAIR IN A HIGHLY DYNAMIC TARGET ENVIRONMENT.

CAPABILITY GAPS:
• MISSION PLANNING SYSTEMS NOT FAST ENOUGH TO ADDRESS TIME CRITICAL TARGETS.
• C3 BETWEEN MISSION PLANNING SYSTEMS, SURVEILLANCE ASSETS, TACAIR, AND CRUISE MISSILES IS INADEQUATE OR DOES NOT EXIST.
• CAPABILITY DOES NOT EXIST TO UPDATE ATR AND AIM POINT SELECTION AFTER LAUNCH IN RESPONSE TO DYNAMIC TARGETS.
• REAL-TIME SUPPORT LACKING FOR ALL-SOURCE TACTICAL INFORMATION PRESENTATION, IN-FLIGHT MISSION REHEARSAL, AND RESOURCE OPTIMIZATION.

OBJECTIVES:

• DEMONSTRATE HIGH ACCURACY FOG IMU ON A HYBRID CHIP USING AWB PIONEERED TECHNOLOGY.

RISK:

• ELECTRO-OPTICAL HYBRID INTEGRATION IS A FIRST.
• POLARIZING WAVEGUIDE
• PHASE MODULATORS
• LIFE-OFF PROCESSES
• PHOTO-VOLTAICS

TECHNICAL APPROACH:
• DEVELOP FABRICATION PROCESSES FOR THE HYBRID CHIP.
• GFE CHIPS TO THE IMU CONTRACTOR.
• INSTRUMENT THE IMU INTO A TEST POD.
• COLLECT DATA AND CALCULATE CEP.
• PREPARE DATA PACKAGE.

OBJECTIVES:

• DEMONSTRATE GPS/MICROMECHANICL IMU GN&C WITH DESPUN CANARD ACTUATOR INTEGRATED IN THE NOSE OF A 5" SHELL.
• SEVERE LAUNCH ENVIRONMENT
  • 9.5 MEGAJOULE GUN—30,000 G, 250 HZ ROLL
  • 18 MEGAJOULE GUN—NEAR 80,000 G

OBJECTIVES:

APPROACH:

OBJECTIVES:

• ADVANCED TECHNOLOGY DEMONSTRATION OF BRASSBOARD REAL-TIME G&C SYSTEM TO LAUNCH ON COORDINATES, MAKE IN-FLIGHT DECISIONS, IDENTIFY TARGETS, AND SELECT AIMPOINTS ON FIXED AND RELOCATABLE TARGETS.

JUSTIFICATION:

TECHNICAL ISSUES:
• INTEGRATE AIMPOINT SELECTION ALGORITHMS WITH LADAR SEEKER AND PREPARE FOR CAPTIVE-CARRY ON F/A-18 OR F-15.
• DEVELOP REAL-TIME PROCESSOR USING OFF-THE-SHELF COMPONENTS TO PERFORM MISSION PLANNING, IMAGE PROCESSING, AND GUIDANCE DECISIONS.

OBJECTIVES:

• DEMONSTRATE AIR-DIRECTED SURFACE-TO-AIR MISSILE (ADSAM) OVER-THE-HORIZON ENGAGEMENT
• USING ELEVATED SENSORS AS A SURROGATE AIR PLATFORM, DETECT, TRACK, ENGAGE, AND KILL OVER-THE-HORIZON CRUISE MISSILE TARGETS.

USE MOUNTAIN TOP SENSORS (RSTER, MK 74 MFCS, CEC) AS SURROGATE AIRBORNE PLATFORM.

• PROVIDE INSIGHTS INTO NEW AIR DEFENSE CONCEPTS OF OPERATIONS.
• JOINT NAVY/ARMY DEMONSTRATION WITH JOINT STAFF AND ALL SERVICE MODELING AND SIMULATION SUPPORT.

RESIDUALS:

• NONE IN PHASE I

• 06-26 JAN 96: ARMY "VIRTUAL ENGAGEMENTS" MISSIONS (SIMULATED FIRING ON TRACK DATA.).
• 20-21 JAN 96: NAVY LIVE MISSILE FIRING TESTS.
• 29 JAN--2 FEB 96: MOUNTAIN TOP ENHANCED JOINT EXERCISE (LITTORAL WARFARE AND DATA COLLECTION)

FUNDING ($M):

TECHNOLOGY:
• EXISTING SURVEILLANCE AND FIRE CONTROL SENSORS (RADAR SURVEILLANCE TECHNOLOGY EXPERIMENTAL RADAR(RSTER) WITH ADS-18S ANTENNA, MK 74 MISSILE FIRE CONTROL SYSTEM, AGEIS PATRIOT RADAR).
• COOPERATIVE ENGAGEMENT CAPABILITY (CEC).
• MODIFIED STANDARD MISSILE (SM-2, BLK III).
• CAPTIVE CARRY PATRIOT PAC-3 MISSILE SEEKER.

PLAYERS:
• USERS: CINCPAC; SERVICE DOCTRINE COMMANDS; U.S. ARMY AIR DEFENSE ARTILLERY SCHOOL
• S&T MANAGERS:
  • NAVY: ONR, PEO(TAD), PMS 400 (AEGIS)
  • ARMY: PEO(MD), PATRIOT
• OTHERS: USAF, USMC, JOINT STAFF, BMDO, ARPA (PLANNING, SIMULATION, CONOPS, DATA COLLECTION)

OBJECTIVES/GOALS:

• MATURE, DEMONSTRATE, AND REDUCE OVERALL RISK OF PRODUCIBLE, TACTICAL BASELINE SMART FUZE.
• INTEGRATE HTSF WITH MMT.
• DEMONSTRATE OPERATIONAL UTILITY OF HTSF.

PAYOFF/MILITARY SIGNIFICANCE:

• SUPPORTS C.P. OF WMD.
• INCREASED SORTIE EFFECTIVENESS AND REDUCED COLLATERAL DAMAGE.
• STREAMLINED ACQUISITION CYCLE.

• ASSEMBLY LINE FACILITIZED 2Q96
• OPERATIONAL UTILITY EVALUATION 2Q96
• CPI PHASE I DEMO 2Q96
• COMPLETE QUAL 3Q96
• FAB/DELIVER 70/16 UNITS 3Q96

FUNDING ($M):

PAST ACCOMPLISHMENTS:
• PRODUCIBLE TACTICAL DESIGN.
• 16 SUCCESSFUL SLED TESTS
• 7 SUCCESSFUL FLIGHT TESTS
• CRITICAL ENVIRONMENTAL QUALITY TESTS
• CONTRACT AWARD—JULY/SEP 95

OBJECTIVES/GOALS:

• DEMO MULTI-MODE WARHEAD IN FLIGHT TEST
  • AEROSTABLE SLUG
  • STRETCHING ROD
  • FRAGMENTS
• DEMO LADAR SENSOR.
  • DETECT, CLASSIFY, TRACK
• DEMO SUBMUNITION MANEUVER PERFORMANCE

PAYOFF/MILITARY SIGNIFICANCE:

• LOW COST/KILL—5 TO 1 IMPROVEMENT.
• INCREASED SORTIE EFFECTIVENESS AND REDUCED COLLATERAL DAMAGE.
• EFFECTIVE MUNITION—SEAD, TMD, JSASM TARGETS, ETC.

• COMPLETE WARHEAD/SUBMUNITION
  INTEGRATION DESIGN 3Q97
• FABRICATE HARDWARE 3Q98
• GROUND TESTING 1Q99
• FLIGHT TESTING 3Q99
• TRANSITION 4Q99

--< SUPPRESSION OF ENEMY AIR DEFENSE (SEAD) WEAPON

FUNDING ($M):

ACCOMPLISHMENTS:
• SENSOR PROVED IN TOWER AND FLIGHT TESTS 1QFY94
• GUIDED FLIGHT TEST (NO WARHEAD) 4QFY94

OBJECTIVES:

• IDENTIFY AND FLIGHT TEST LOW COST ANTIJAM CAPABILITY FOR JDAM TYPE WEAPONS
  • LAB AND ANECHOIC CHAMBER TESTING OF EXISTING OR NEAR-TERM DEVELOPMENTAL ANTIJAM CAPABILITY
  • INTEGRATE AJ TECHNOLOGY INTO SUITABLE CARRIER VEHICLES
  • CONDUCT AJ GPS/INS FLIGHT TEST AT HOLLOMAN AFB, NM

PAYOFF/MILITARY SIGNIFICANCE:

• ANTIJAM CAPABILITY PERMITS GPS ACCURACY FROM WEAPON LAUNCH TO IMPACT
• INCREASED ACCURACY AND EFFECTIVENESS REDUCES NUMBER OF AIRCRAFT SORTIES REQUIRED

• COMPLETE SUBSYSTEM TESTING 2Q96
• COMPLETE INTEGRATION 2Q97
• COMPLETE GROUND TESTING 4Q97
• COMPLETE FLIGHT TESTING 2Q98
• TRANSITION TO JDAM PIP 1Q99

ACCOMPLISHMENTS:
• SPATIAL/TEMPORAL DISCRIMINATION OF JAMMER 2Q93
• THAGG HARDWARE FABRICATED 4Q94