C-80_Script_5-1-14_TAIP_-_updated.pdf
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- Attached to
- Eglin Operations & Maintenance Services (Formerly Eglin Test & Training Complex Technical Services (ETTC-TS) Program) Federal contract opportunity
- Solicitation number
- FA2486-16-R-0002
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C-80 Script
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Distribution Statement A: Approved for public release; distribution is unlimited.
C-80 COMPLEX
(IN FRONT OF C-80C)
EGLIN OPERATION AND MAINTENANCE
SERVICES
(E-OMS) INDUSTRY DAYS
4 JUNE 2014
WELCOME TO THE C-80 COMPLEX, COMMONLY KNOWN
AS THE ARENA TEST COMPLEX. THE COMPLEX CONSISTS OF
4 TEST AREAS AND SUPPORTS A WIDE RANGE OF MUNITIONS
TESTING INCLUDING ARENA, INSENSITIVE MUNITIONS, STATIC
DETONATION AND OPERATIONAL GROUND TESTING. WE ARE
LOCATED AT C-80C.
C-80C
C-80C IS OUR PRIMARY JMEMS ARENA TEST FACILITY.
TESTS ARE STRICTLY RUN ACCORDING TO JOINT MUNITION
EFFECTIVENESS MANUAL (JMEM) TO ACCURATELY
CHARACTERIZE THE MUNITIONS EFFECTIVENESS AND
SAFETY. TYPICAL TESTS INCLUDE VERTICAL AND
HORIZONTAL WEAPON ORIENTATIONS. THIS DATA IS INPUT
IN MODELS TO SIMULATE THE WEAPON’S EFFECTIVENESS
AGAINST A VARIETY OF TARGETS. THIS RANGE IS
INSTRUMENTED TO COLLECT BLAST PRESSURE, TIME OF
FRAGMENT ARRIVAL, AND HIGH-SPEED AND STANDARD
RATE VIDEO DATA. XYZ SCORING OF FRAGMENTS IS
PERFORMED MANUALLY.
A TYPICAL ARENA TEST INCLUDES FRAGMENT IMPACT
BUNDLES, ARRANGED IN A CIRCULAR ARENA TO RECORD A
FRAGMENT’S LOCATION AND DEPTH OF PENETRATION.
VELOCITY AND TIME OF FRAGMENT ARRIVAL DATA IS
PROVIDED BY VELOCITY SCREENS ATTACHED TO THE FRONT
OF THE FRAGMENT IMPACT BUNDLES. BLAST PRESSURE
TRANSDUCERS ARE POSITIONED ON RADIALS TO RECORD
PRESSURE DATA AT DISTANCES AWAY FROM DETONATION.
THE X-Y-Z DATA IS SCORED POST MISSION BY SITE
PERSONNEL AND THE FRAGMENTS ARE RECOVERED,
CLEANED, AND WEIGHED AT C-80W.
THIS FACILITY CAN TEST MUNITIONS WITH NET
EXPLOSIVE WEIGHTS UP TO 3,000 LBS. THIS CONCLUDES
THE C-80C TOUR.
C-80W
(LOCATED AT INTERSECTION OF RR201 AND RR214)
TO OUR RIGHT IS C-80W. C-80W PROVIDES A
CALIBRATION AREA FOR A WIDE RANGE OF TRANSDUCER
AND SIGNAL CONDITIONING EQUIPMENT THAT IS TRACEABLE
TO NATIONAL INSTITUTE OF STANDARDS AND TECHNOLOGY
(NIST) STANDARDS. TYPICAL TRANSDUCERS INCLUDE:
PRESSURE, ACCELEROMETERS, STRAIN GAUGES,
MICROPHONES, LOAD CELLS, PIEZOELECTRIC PINS AND
FORCE RINGS.
INSIDE STORAGE IS AVAILABLE FOR MATERIALS
REQUIRED TO CONDUCT JMEMS TESTING.
VELOCITY SCREENS ARE USED TO MEASURE
FRAGMENT VELOCITY FOR ARENA TESTING. AN ALUMINUM
OXIDE FLAME SPRAY SYSTEM IS AVAILABLE TO SPRAY
CONDUCTIVE MATERIAL ON A CARDBOARD BASE TO
PROVIDE FRAGMENT ARRIVAL DATA FOR VELOCITY
MEASUREMENTS.
JMEM STANDARDS REQUIRE FRAGMENT LOCATION AND
SIZE MEASUREMENTS. A BEAD BLASTER IS EMPLOYED TO
CLEAN FRAGMENTS, AND A COMPUTER-CONTROLLED
FRAGMENT WEIGHING SYSTEM IS USED TO RECORD
LOCATIONS AND WEIGHTS.
THE EXPLOSIVE INSTRUMENTATION DATA SYSTEM OR
EIDS VANS ARE MOBILE INSTRUMENTATION PLATFORMS TO
CONDUCT EXPLOSIVE TESTING. THE EIDS VANS PROVIDE A
WIDE RANGE OF TRANSDUCERS, DATA COLLECTION
SYSTEMS, SIGNAL CONDITIONERS, AND FIRING SYSTEMS TO
ACCOMPLISH THE MISSION. THESE SYSTEMS ARE USED ON
THE C-80 COMPLEX, BUT MAY ALSO BE DEPLOYED TO
REMOTE TEST AREAS ON EGLIN, AND REMOTE TDY
LOCATIONS. THE EIDS VANS HAVE RADIO REMOTE FIRING
SYSTEM CAPABILITIES USED TO FIRE ITEMS WITH A LARGE
SAFETY FOOTPRINT. THE SYSTEM PROVIDES A RADIO-
LINKED FIRING SUPPLY AND CONTROL SYSTEM USED TO
FIRE ITEMS AND KEEP THE OPERATORS OUT OF THE SAFETY
FOOTPRINT.
C-80A
DOWN THIS ROAD TO THE SOUTH IS C-80A, ALSO
KNOWN AS THE OPERATIONAL GROUND TEST FACILITY
(OGT). OUR OGT FACILITY IS USED TO PERFORM NON-
DESTRUCTIVE TESTING ON ALL UP ROUNDS IN A SIMULATED
ENVIRONMENT. THE TEST ITEM IS SUBJECTED TO
ENVIRONMENTAL CONDITIONS THAT WOULD BE
ENCOUNTERED DURING A TYPICAL OPERATIONAL FLIGHT
MISSION. THERE ARE 4 PHASES SIMULATED DURING A
TYPICAL TEST MISSION: TAXI/TAKEOFF, CAPTIVE CARRY,
FREE-FLIGHT, AND TERMINAL APPROACH. TEMPERATURE,
VIBRATION, AND SHOCK ARE USED TO SIMULATE THE
TAXI/TAKEOFF AND CAPTIVE CARRY PORTIONS OF THE TEST
ENVELOPE. ENGINE RUN AND SCENE GENERATION
SIMULATIONS ARE USED TO SIMULATE THE FREE-FLIGHT
AND TERMINAL APPROACH PORTIONS. SIMULATIONS
INCLUDE INFRARED, RF, VISIBLE, AND GPS. THE OGT IS A
TEST APPROACH, AND CAN BE CONDUCTED AT OTHER
LOCATIONS FOR INERT ITEMS INCLUDING MCKINLEY
CLIMATIC LAB AND JPRIMES. EXPLOSIVE ITEMS THAT
CANNOT HAVE THE WARHEAD REMOVED MUST BE TESTED
HERE.
THE TEST CHAMBER HOUSES THE ENVIRONMENTAL
CONDITIONING, VIBRATION AND SENSORS REQUIRED TO
CONDUCT OGT MISSIONS. NORTH OF THIS FACILITY IS THE C-
80A CONTROL BUNKER. THIS BUNKER HOUSES THE
CONTROL, INSTRUMENTATION AND VIDEO SYSTEMS
REQUIRED TO OPERATE THE SITE WHILE LIVE ITEM TESTING
IS BEING PERFORMED.
THE CHAMBER PROVIDES A CONTROLLED
ENVIRONMENT TO CONDUCT OGT. A 50,000-FORCE POUND
VIBRATION SYSTEM PROVIDES THE SPECIFIC VIBRATION
PROFILE THE WEAPON WILL BE EXPECTED TO ENDURE
UNDER A FLIGHT TEST. TWO ADDITIONAL 20,000 FORCE
POUND VIBRATION SYSTEMS ARE ALSO AVAILABLE AT THIS
SITE. TWO TEMPERATURE CONDITIONING SYSTEMS ARE
USED TO PROVIDE CONDITIONED AIR TO AN INSULATED
ENCLOSURE BOX DURING THE TESTING. AN ITEM WILL
TYPICALLY BE CONDITIONED FOR A PERIOD OF 12-18 HOURS
PRIOR TO TEST EXECUTION. TO MORE ACCURATELY
SIMULATE THE DYNAMICS OF A CAPTIVE CARRY PROFILE,
ACTUAL AIRCRAFT WINGS ARE SOMETIMES USED TO
PERFORM THE TEST.
THE VIBRATION SYSTEM AND TEMPERATURE
CONDITIONING SYSTEMS REQUIRE CHILLED WATER FOR
COOLING. THE FACILITY HAS A WATER CHILLER SYSTEM
INSTALLED TO ACCOMPLISH THIS FUNCTION.
AFTER THE TEMPERATURE/VIBRATION CYCLE IS
COMPLETE, THE TEST TRANSITIONS TO SCENE GENERATION
AND ENGINE RUN TO SIMULATE FREE-FLIGHT AND TERMINAL
APPROACH. HARDWARE-IN-THE-LOOP SIMULATIONS ARE
USED TO PROVIDE THE APPROPRIATE SCENE TO THE
SEEKER UNDER TEST. THE SIMULATIONS AND EQUIPMENT
ARE PROVIDED BY PERSONNEL AT THE GWEF AND JPRIMES.
WHILE THE SIMULATIONS ARE RUNNING, THE ENGINE OR
ROCKET MOTOR IS STARTED, AND SEEKER SIGNALS ARE
RECORDED TO DETERMINE WEAPON PERFORMANCE. THIS
DATA IS PROVIDED TO ANALYSTS FOR EVALUATION.
ITEMS USING JET FUEL CAN BE TESTED INSIDE THIS
CHAMBER. ROCKET FUELED ITEMS MUST BE TESTED
OUTSIDE ON AN ENGINE RUN STAND.
THE ENGINE RUN STAND IS CONFIGURED TO USE THE
ACTUAL HARDWARE FROM INVENTORY AIRCRAFT TO MORE
ACCURATELY TEST MUNITIONS. THE STAND IS
INSTRUMENTED TO PROVIDE THRUST DELIVERED FROM THE
ROCKET MOTOR. SCENE GENERATION EQUIPMENT IS
PLACED IN APPROPRIATE POSITIONS TO PROVIDE
STIMULATION TO THE SEEKER. HIGH-SPEED VIDEO AND
STANDARD RATE VIDEO IS USED TO OBSERVE THE
OPERATION OF THE ITEM DURING THE TEST. FIBER-OPTIC
LINKS ARE ESTABLISHED BETWEEN THE TEST CHAMBER
AND THE CONTROL BUNKER FOR SEEKER SIGNAL DATA.
THIS CONCLUDES THE C-80 COMPLEX TOUR.
File details come from the government source that posted it. Updated .