Attachment_2_-_IFF_Antenna_VCRM.xlsx
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- Solicitation number
- M67854-17-R-6001
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United States Marine Corps
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VCRM
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PQT VCRM
| 5-Apr-17 | Verification Method | Verification Reference | Verification Method | Verification Reference | ||||||||||||||||||||||
| Requirements | Performance Qualification Test (PQT) Test Objective | PQT Test Procedure | (A) Analysis | (I) Inspection | (D) Demo | (T) Test | Verification Results | (A) Analysis | (I) Inspection | (D) Demo | (T) Test | Verification Results | ||||||||||||||
| Met: | Met: | |||||||||||||||||||||||||
| Met with Exception (MWE): | Met with Exception (MWE): | |||||||||||||||||||||||||
| Not Met: | Not Met: | |||||||||||||||||||||||||
| LOC Reference | Description | A-Spec Reference | Description | PIDS | Description | Performance Spec Reference | Description | Derived Requirement # | Description | Test Objective # | Description | Test Procedure # | Description | Not Yet Evaluated (NYE): | Not Yet Evaluated (NYE): |
| PQT | Validated By | FUE | Validated By | |||||||||||||
| 1.4.1 | 17 | The radar system shall be capable of integrating an Identification Friend or Foe (IFF) system, with an integrated IFF antenna, utilizing ancillary GFE with a 180nmi threshold range. | A-1306 | The system shall[] interface to the GFE IFF Subsystem equipment to provide the IFF capabilities required herein, to include interfacing to the IFF Subsystem in accordance with Ethernet Design Specification WS-34034 (AN/UPX-24A), Interface Control Document TBD (IFF Subsystem), and Installation Control Drawing TBD (Interrogator Set AN/UPX-41(C)). | ATG-491 | The ATG shall[] provide two channels of IFF RF transmission line cabling from the ATG Interface to the slip ring and from the slip ring to the IFF Antenna | ||||||||||
| 17 | The radar system shall be capable of integrating an Identification Friend or Foe (IFF) system, with an integrated IFF antenna, utilizing ancillary GFE with a 180nmi threshold range. | A-301 | The system shall[] support IFF interrogation in the 5 second and 10 second rotation rates | ATG-109 | ATG-109 The ATG shall[] support an IFF sub system interrogation capability for synchronous rotation with the Primary Radar. | 3.1.1 | The IFF Antenna shall provide three independent beams (threshold): (1) Interrogate/Monopulse SUM for transmit and receive, (2) Side Lobe Suppression (SLS or Control) for transmit and receive, (3) Monopulse Difference for receive (threshold). | X | ||||||||
| 3.1.2 | The Interrogate and SLS characteristics shall apply to the frequency range 1026.5 MHz to 1033.5 MHz (threshold) | X | ||||||||||||||
| 3.1.3 | The SUM, SLS and Difference characteristics shall apply to the frequency range 1085 MHz to 1095 MHz (threshold). | X | ||||||||||||||
| 3.1.4 | The radiation at the SUM port, SLS port and Difference port shall be linearly polarized with Vertical Polarization (threshold). | X | ||||||||||||||
| 3.1.5 | The Cross Polarization at the SUM port shall be greater than 20 decibel (dB) (threshold) at the main beam. | X | ||||||||||||||
| 3.1.6 | The peak antenna gain at the SUM input port shall be at least 22 Decibels Above Isotropic (dBi) (threshold) and 24 dBi (objective). | X | ||||||||||||||
| 3.1.7 | The peak transmit power at antenna SUM port shall be 10 kW (threshold). | X | ||||||||||||||
| 3.1.8 | The average transmit power at antenna SUM port shall be 100 W (threshold). | X | ||||||||||||||
| 3.1.9 | The peak input power at antenna SLS port shall be 10 kW (threshold). | X | ||||||||||||||
| 3.1.10 | The average input power at antenna SLS port shall be 100 W (threshold). | X | ||||||||||||||
| 3.1.11 | The SUM pattern’s horizontal 3-dB beam width shall be 4.5 ± 0.5 degrees (threshold) and 3.5 degrees nominal (objective). | X | ||||||||||||||
| 3.1.12 | The SUM pattern’s horizontal side-lobe level, below the peak main beam, shall be greater than 25 dB (threshold). | X | ||||||||||||||
| 3.1.13 | The SUM pattern’s vertical 3-dB beam width shall be 25.5 ± 3.0 degrees (threshold). | X | ||||||||||||||
| 3.1.14 | The SUM pattern’s vertical side-lobe level, below the peak main beam, shall be greater than 18.0 dB (threshold). | X | ||||||||||||||
| 3.1.15 | The isolation between SUM and Difference ports shall be greater than 28 dB (threshold). | X | ||||||||||||||
| 3.1.16 | The maximum Voltage Standing Wave Ratio (VSWR) at the SUM port shall be 1.5:1 (threshold). | X | X | |||||||||||||
| 3.1.17 | The maximum VSWR ratio at the Difference port shall be 1.5:1 (threshold). | X | X | |||||||||||||
| 3.1.18 | The maximum VSWR ratio at the SLS port shall be 1.5:1 (threshold). | X | X | |||||||||||||
| 3.1.19 | The IFF Antenna shall support the IFF Modes 1, 2, 3, 4, 5 (Level 1 & 2 (threshold)), C, and S (Level 1 & 2 (threshold)) for a 360-degree’s rotation in the 6 Revolutions Per Minute (RPM) and 12 RPM rotation rates of the Primary Search Antenna. | X | ||||||||||||||
| 3.1.20 | 3.1.20 The IFF Antenna input/output connectors shall be female N-type, MIL-C-39012 (threshold) to accommodate three (3) channels output. | X | ||||||||||||||
| 3.1.21 | The IFF Antenna dimensions shall not exceed 180” L x 35” H x 26” W (threshold). | X | ||||||||||||||
| 3.1.22 | The IFF Antenna with mount shall not exceed 150 pounds (threshold) 115 pounds (objective). | X | ||||||||||||||
| 3.1.23 | The IFF Antenna shall mount to the support frame of the AN/TPS-59A(V)3 Radar Antenna Array and accommodate the existing Auxiliary (AUX) antenna, lightning rods and aircraft warning lights (threshold). | X | ||||||||||||||
| 59 | Shielding shall be required to allow the radar to operate while encountering the levels of electromagnetic interference (EMI) that would be found in the worst case threat environment and to prevent the unintentional radiation of electromagnetic signals from the radar. | A-387 | The system shall[] operate within the electromagnetic interference (EMI) emission susceptibility limits system self-compatibility limits in accordance the requirements associated with CE102, CS101, CS114,RE102 and RS103 of MIL-STD-461 | ATG-187 | The ATG shall[] operate within the electromagnetic interference (EMI) emission susceptibility limits system self-compatibility limits in accordance the requirements associated with CE102, CS101, CS114, RE102 and RS103 of MIL-STD-461 | 3.3.1 | The IFF Antenna shall operate within the EMI emission susceptibility limits and self-compatibility limits in accordance the requirements associated with CE102, CS101, CS114, RE102 and RS103 of MIL-STD 461G (threshold | X | X | |||||||
| 61 | Grounding of the system components shall be sufficient to insure that no personal injury or damage to system components results from stray voltages or static discharges. | A-365 | The system shall[] be designed to prevent personnel hazards involving electronic equipment safety design criteria in accordance with Requirement 1 of MIL-HDBK-454 and MIL-STD-882. | ATG-494 | The ATG shall[] be designed to prevent personnel hazards involving electronic equipment safety design criteria in accordance with MIL-HDBK-454 and MIL-STD-1472. | 3.3.2 | The IFF antenna system provider shall protect from hazardous effects of electromagnetic radiation by specifying safe stand-off distances and by providing appropriate equipment labeling for Hazards of Electromagnetic Radiation to Ordnance, Hazard of Electromagnetic Radiation to Personnel, and Hazard of Electromagnetic Radiation to Fuel in accordance with DODI 6055.11 and Marine Corps Order 5104.2 and MIL-STD-464 | X | X | |||||||
| N/A | N/A | A-708 | Exposed metal surfaces of the IFF antenna shall[] be painted in accordance with MIL-C-53039 or MIL-DTL-53039 with coating of color FED-STD-595 Color #34094 (Green 383). | ATG-259 | Exposed metal surfaces of the IFF antenna shall[] be painted in accordance with MIL-C-53039 or MIL-DTL-53039 with coating of color FED-STD-595 Color #34094 (Green 383). | 3.4.1 | Exposed metal surfaces of the IFF antenna shall be painted in accordance with MIL-C-53039 or MIL-DTL-53039, with coating of FED-STD-595 Color #34094 (Green 383) (threshold). | X | ||||||||
| 35 | The radar system shall withstand pressures and maintain all seals in the operating condition normally encountered at elevations from sea level to 10,000 feet (3.05 km) Above Sea Level (ASL | A-389 | The system shall[] operate at altitudes between -300 feet and 10,000 feet above sea level | ATG-189 | The ATG shall[] operate at altitudes between -300 feet and 10,000 feet above sea level. | 3.4.2 | The IFF Antenna shall operate at altitudes between -300 feet and up to 10,000 feet above sea level (threshold). | 5l | X | X | ||||||
| 39 | The radar system shall be capable of normal operation in winds of 50 knots, degraded operation in winds of 75 knots, surviving with the array lowered in winds of 100 knots, and capable of surviving winds of 120 knots in the transport condition. | A-392 | The system shall[] be capable of operation in wind speeds up to 50 knots. | ATG-191 | The ATG shall[] be capable of Normal operation in wind speeds up to 50 knots. | 3.4.3 | The IFF Antenna shall be capable of normal operation in wind speeds up to 50 knots (threshold). | X | X | |||||||
| 40 | The radar system shall be capable of operation when the antenna is subjected to winds up to 75 knots with up to 3.5 pounds per square foot of antenna ice loading. | A-393 | The system shall[] be capable of degraded operation of no more than 2dB (due to antenna speed, tilt, and array surface variation) in wind speeds up to 75 knots and with up to 3.5 pounds per square foot of ice loading. | ATG-192 | The ATG shall[] be capable of degraded operation of no more than 2dB, worst case, due to the combined effects of antenna speed, tilt, and array surface variation in wind speeds up to 75 knots and with up to 3.5 pounds per square foot of ice loading | 3.4.4 | The IFF Antenna shall be capable of degraded operation of no more than 2 dB (due to antenna speed, tilt, and array surface variation) in wind speeds up to 75 knots and with up to 3.5 pounds per square foot of ice loading (threshold). | X | X | |||||||
| 42 | The radar system shall be capable of operating in a maximum rainfall of 5/8 inches per hour. | A-397 | The system shall[] be capable of operation in rainfall of at least 0.625 inch per hour | ATG-196 | The ATG shall[] be capable of operation in rainfall of at least 0.625 inch per hour. | 3.4.5 | The IFF Antenna shall be capable of operation in rainfall of at least 0.625 inch per hour (threshold). | X | X | |||||||
| 30 | The equipment shall be capable of continuing to operate if the outside ambient temperature falls to -40 degrees Fahrenheit (F) or rises to +122 degrees F (-40 degrees Celsius to +50 degrees Celsius). | A-398 | The system shall[] be capable of operation and transport between -40°and +50° Celsius. | ATG-197 | The ATG shall[] be capable of operation and transport between -40 and 50 +Celsius. | 3.4.6 | The IFF Antenna shall be capable of operation between -40 degrees and +50 degrees Celsius (threshold). | X | X | |||||||
| 32 | The equipment shall be capable of being stored or transported without being rendered inoperative in an ambient temperature of -40 degrees F to +160 degrees F (-40 degrees Celsius to 71 degrees Celsius). | A-399 | The system shall[] be capable of storage between -40°and +71° Celsius | ATG-198 | The ATG shall[] be capable of storage between -40 and +70.9 Celsius. | 3.4.7 | The IFF Antenna shall be capable of storage between -40 degrees and +71 degrees Celsius (threshold | X | X | |||||||
| 43 | The radar system shall be capable of operating and withstanding a maximum of 99% humidity, and of withstanding a maximum of 99% relative humidity when the equipment is stored. The objective and threshold are the same. The radar system must operate, be transported, and survive in these environmental conditions without becoming unsafe or inoperative due to fatigue or failure when prescribed maintenance procedures are followed. | A-400 | The system shall[] be capable of operation, transport, and storage in relative humidity up to 95%, where above +27° Celsius, the relative humidity is based upon a dew point of +27° Celsius | ATG-199 | The ATG shall[] be capable of operation, transport, and storage in relative humidity up to 95%, where above +27 Celsius, the relative humidity is based upon a dew point of +27 Celsius | 3.4.8 | The IFF Antenna shall be capable of operation, transport, and storage in relative humidity up to 95%, where above +27 degrees Celsius; the relative humidity is based upon a dew point of +27 degrees Celsius (threshold). | 5r | X | X | ||||||
| 38 | The radar system shall operate, be transported, and survive in these environmental conditions without becoming unsafe or inoperative due to corrosion or fatigue when prescribed maintenance procedures are followed. | A-401 | The system finishes and coatings on components and system structures shall[] survive after exposure to a salt fog environment without suffering corrosion damage that would render the system inoperable in accordance with the salt fog test of MIL-STD-810. | ATG-404 | The ATG finishes and coatings on components and system structures shall[] survive after exposure to a salt fog environment without suffering corrosion damage that would render the system inoperable in accordance with the salt fog test of MIL-STD-810. | 3.4.9 | The IFF Antenna’s finishes and coatings on components shall allow them to endure exposure to a salt fog environment without suffering corrosion damage that would render the antenna inoperable in accordance with the salt fog test of MIL-STD-810G (threshold). | 5s | X | X | ||||||
| N/A | N/A | A-402 | The system shall[] meet all system performance requirements when exposed to sand and dust particles in accordance with the sand and dust test of MIL-STD-810. | ATG-405 | The ATG shall[] meet all system performance requirements when exposed to sand and dust particles in accordance with the sand and dust test of MIL-STD-810. | 3.4.10 | The IFF Antenna shall meet IFF performance requirements when exposed to sand and dust particles in accordance with the sand and dust test of MIL-STD-810G (threshold). | X | X | |||||||
| N/A | N/A | A-683 | All connectors, fuse covers, and captivated fittings hardware exposed to the weather shall[] be furnished with covers to prevent the entrance of dirt and water into the connectors when the plug and jack are not mated. | ATG-231 | All connectors, fuse covers, and captivated fittings hardware exposed to the weather shall[] be furnished with covers to prevent the entrance of dirt and water into the connectors when the plug and jack are not mated. | 3.4.11 | 1.1.4 All connectors shall be supplied with captive hardware to prevent connector damage and the entrance of moisture and foreign material during storage (threshold). | X | ||||||||
| 51 | Availability is a measure of the degree to which a system is in an operable and committable state at the start of a mission, given a random point in time. The threshold shall be 700 hours of the 720 hour employment, with no more than 2 consecutive hours of non-availability for corrective or planned maintenance, not counting delays due to administration or logistics | A-775 | The Mean Time Between Critical Failures (MTBCF) of the system shall[] be equal to or greater than 2,000 hours | ATG-290 | The ATG shall[] support the system level requirements of the Mean Time Between Critical Failures (MTBCF). | 3.9.1 | The IFF Antenna shall have a Mean Time Between Failure and Mean Time Between Critical Failure (MTBCF) of 125,000 hours (threshold | X | ||||||||
| N/A | N/A | A-840 | The system shall[] be designed for a 15-year service life with refurbishment at 5-year intervals. | ATG-341 | The ATG shall[] be designed for a 15-year service life with refurbishment at 5-year intervals | 3.9.2 | The IFF Antenna shall have a minimum of 15-year life span of being able to meet all IFF performance requirements without the need for scheduled depot maintenance (objective | X | ||||||||
| 61 | Grounding of the system components shall be sufficient to insure that no personal injury or damage to system components results from stray voltages or static discharges. | A-365 | The system shall[] be designed to prevent personnel hazards involving electronic equipment safety design criteria in accordance with Requirement 1 of MIL-HDBK-454 and MIL-STD-882. | ATG-494 | The ATG shall[] be designed to prevent personnel hazards involving electronic equipment safety design criteria in accordance with MIL-HDBK-454 and MIL-STD-1472. | 3.10.1 | The IFF antenna assembly shall be designed to prevent personnel hazards involving electronic equipment safety design criteria in accordance with MIL-HDBK-454 and MIL-STD-882 (threshold). | X | ||||||||
| 23 | The radar system shall be transportable | A-864 | The IFF antenna shall[] be capable of being removed from the primary search radar antenna for transport | ATG-140 | The IFF antenna shall[] be capable of being removed from the primary search radar antenna for transport. | 3.10.2 | The IFF Antenna shall be designed for human engineering design criteria and principles in accordance with MIL-STD-1472D (threshold | X | ||||||||
| 23 | The radar system shall be transportable | A-865 | No single section or combination of sections of the IFF antenna, mounting hardware, and transport packaging that must be moved singularly or together during assembly, disassembly or transport shall[] weigh more than 85 pounds | ATG-141 | No single section or combination of sections of the IFF antenna and accompanying mounting hardware and transportation packaging (that must be moved singularly or together during assembly, disassembly or transport) shall[] weigh more than 85 pounds. | 3.12.1 | The IFF Antenna shall be capable of removal from the Primary Search Radar Antenna for transport (threshold). | X | X | |||||||
| 23 | The radar system shall be transportable | A-866 | During transport the IFF antenna assemblies shall[] be stored within and secured to the shelters in a manner that prevents damage to the IFF antenna and other components | ATG-142 | During transport the IFF antenna assemblies shall[] be stored within and secured to the shelters in a manner that prevents damage to the IFF antenna and other components. | 3.12.2 | The IFF Antenna shall dis-assemble into multiple sections for transportation in an S-280 shelter floor loaded (threshold). | X | X | |||||||
| 29 | The equipment shall withstand the vibration and shock encountered in the loading and movement by the above [highway, rail, marine, and air modes] transportation modes. | A-855 | In the Transport Configuration, the system shall[] be designed to meet the transit drop requirements in accordance with MIL-STD-810, without deterioration of performance | ATG-345 | In the Transport Configuration, the ATG shall[] be designed to meet the transit drop requirements in accordance with MIL-STD-810, without deterioration of performance. | 3.12.3 | The IFF Antenna shall have reusable ruggedized storage containers with carrying handles for two-person carry and anchor points for stowage and shipment (threshold). | X | ||||||||
| 23 | The radar system shall be transportable | A-866 | During transport the IFF antenna assemblies shall[] be stored within and secured to the shelters in a manner that prevents damage to the IFF antenna and other components | ATG-142 | During transport the IFF antenna assemblies shall[] be stored within and secured to the shelters in a manner that prevents damage to the IFF antenna and other components. | 3.12.4 | The floor loading storage space for all IFF Antenna containers shall not exceed 114” L x 19” W x 48” H (threshold). | X | ||||||||
| 36 | The radar system shall not be rendered inoperative in the transport condition at an altitude of 45,000 feet (13.7 km) ASL. The threshold and the objective are the same. | A-391 | The system shall[] survive unpressurized transport at altitudes up to 45,000 feet above sea level | ATG-190 | The ATG shall[] survive unpressurized transport at altitudes up to 45,000 feet above sea level. | 3.12.5 | The IFF Antenna shall be transportable unpressurized at altitudes up to 45,000 feet (threshold). | X | ||||||||
| 23 | The radar system shall be transportable | A-865 | No single section or combination of sections of the IFF antenna, mounting hardware, and transport packaging that must be moved singularly or together during assembly, disassembly or transport shall[] weigh more than 85 pounds | ATG-141 | No single section or combination of sections of the IFF antenna and accompanying mounting hardware and transportation packaging (that must be moved singularly or together during assembly, disassembly or transport) shall[] weigh more than 85 pounds. | 3.12.6 | No single section or combination of sections of the IFF antenna, mounting hardware, and transport packaging that must be moved singularly or together during assembly, disassembly or transport shall weigh more than 85 pounds (threshold) | X | ||||||||
| 61 | Grounding of the system components shall be sufficient to insure that no personal injury or damage to system components results from stray voltages or static discharges. | A-365 | The system shall[] be designed to prevent personnel hazards involving electronic equipment safety design criteria in accordance with Requirement 1 of MIL-HDBK-454 and MIL-STD-882. | ATG-494 | The ATG shall[] be designed to prevent personnel hazards involving electronic equipment safety design criteria in accordance with MIL-HDBK-454 and MIL-STD-1472. | 3.13.1 | The standards for workmanship shall meet MIL-HDBK-454B (threshold). | X | ||||||||
| N/A | N/A | N/A | N/A | N/A | N/A | 3.13.2 | The Contractor shall comply with the Prohibited, Restricted and Hazardous Materials listed in NAS 411-1 | X |
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