Attachment_(2)_-_CLRF_IC_CPSCM__MSC_-_1_Aug_2014.xlsx

XLSX spreadsheet 46 KB Posted Aug 13, 2014

Attached to: COMMON LASER RANGE FINDER INTEGRATED CAPABILITY
Solicitation number: M67854-14-R-6001
Issued by: United States Marine Corps

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Attachment (2) - CLRF_IC_CPSCM__MSC - 1 Aug 2014

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File	Type	Posted
M67854-14-R-6001_0003.doc	DOC document	Aug 22, 2014
Attachment_(7)_-_Section_B_-_Description_of_Supplies_Services_18_Aug_14.xlsx	XLSX spreadsheet	Aug 18, 2014
M67854-14-R-6001_0002.doc	DOC document	Aug 18, 2014
Attachment_(1)_-_CLRF_IC_Performance_Specification_3_Jul_2014.docx	DOCX document	Aug 13, 2014
Attachment_(7)_-_Section_B_-_Description_of_Supplies_Services_-_7_Aug_14.xlsx	XLSX spreadsheet	Aug 13, 2014
Exhibits_(A)-(C)_-_CLRF_IC_Production_CDRLs_1_Aug_2014.pdf	PDF	Aug 13, 2014
Attachment_(9)_-_CLRF_IC_Final_RFP_Questions_ _Answers_-_8_Aug_2014.xlsx	XLSX spreadsheet	Aug 13, 2014
M67854-14-R-6001_0001.doc	DOC document	Aug 13, 2014
Attachment_(1)_-_CLRF_IC_Performance_Specification_3_Jul_2014.pdf	PDF	Jul 15, 2014
Attachment_(7)_-_Section_B_-_Description_of_Supplies_Services_15_Jul_14.xlsx	XLSX spreadsheet	Jul 15, 2014
Attachment_(2)_-_CLRF_IC_CPSCM__MSC_15_Jul_2014.xlsx	XLSX spreadsheet	Jul 15, 2014
Attachment_(8)_-_Past_Performance_Questionnaire_16_Jun_2014.docx	DOCX document	Jul 15, 2014
Attachment_(6)_-_CLRF_IC_GFP_16_Jun_2014.pdf	PDF	Jul 15, 2014
Attachment_(4)_-_CLRF_IC_FDA_Compliance_Checklist_1_Jul_2014.pdf	PDF	Jul 15, 2014
Attachment_(3)_-_CLRF_IC_CRM_Template_16_Jun_2014.xlsx	XLSX spreadsheet	Jul 15, 2014
Exhibits_(A)-(C)_-_CLRF_IC_Production_CDRLs_9_Jul_2014.pdf	PDF	Jul 15, 2014
Attachment_(5)_-_DD254_M67854-14-R-6001_27_Jan_2014.pdf	PDF	Jul 15, 2014
CLRF_IC_FINAL_RFP_M67854-14-R-6001_15_JUL_2014.doc	DOC document	Jul 15, 2014
CLRF_IC_Draft__RFP_Questions_Answers_-_1_Jul_14.pdf	PDF	Jul 1, 2014
DRAFT_CLRF_IC_Section_B_-_Description_of_Supplies_Services_5_Jun_14.xlsx	XLSX spreadsheet	Jun 12, 2014
DRAFT_CLRF_IC_Sections_L_ _M_12_Jun_14.docx	DOCX document	Jun 12, 2014
DRAFT_CLRF_IC_Section_F_Delivery_Requirements_5_Jun_2014.docx	DOCX document	Jun 12, 2014
DRAFT_CLRF_IC_Section_H_Clause_-_Government_Purpose_Rights_12_Jun_14.docx	DOCX document	Jun 12, 2014
DRAFT_CLRF_IC_Performance_Specification_20140609.docx	DOCX document	Jun 10, 2014
DRAFT_CLRF_IC_Production_SOW.docx	DOCX document	Jun 10, 2014
DRAFT_CLRF_IC_Production_CDRLs.docx	DOCX document	Jun 10, 2014

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CPSCM

		Perf Spec Para	Government CLRF IC Light Performance Specification	Compliance:
Fails to Meet Threshold, Threshold, Exceed Threshold, Objective, Not Applicable	Proposed Performance:

Chapter 3: If other than "Threshold" or "Objective," state proposed performance, why your design fails to meet Threshold, or why this requirement is Not Applicable.

Chapter 4: State "Compliant" or explain deviations and why.

Nominal Mission Profile			3.1	The nominal mission profile for the CLRF IC is 72 hours. During the mission, the CLRF IC system will be operated for three six-hour periods. Half of the operating hours (9 total hours) will occur during daylight, the other half of the operating hours (9 total hours) will occur at night. A total of 75 targeting measurement/data export operations will be performed. It is acceptable to change the battery set twice during a nominal mission profile and the additional batteries will not count towards the CLRF IC system weight.
			4.9.1	The ability of the CLRF IC to conform to the requirements specified in 3.1 shall be verified through analysis and demonstration.
Weight			3.2	The CLRF IC, including the one set of batteries and battery cartridge inside the system, a carrying strap, and lens covers shall be no more than 3.0 lbs (Threshold). Note: this weight requirement must be met with the battery type and cartridge which meets the battery life requirements in paragraph 3.15.6. This weight does not include ancillary items.
				The CLRF IC, including the one set of batteries and battery cartridge inside the system, a carrying strap, and lens covers shall be no more than 2.75 lbs (Objective). Note: this weight requirement must be met with the battery type and cartridge which meets the battery life requirements in paragraph 3.15.6. This weight does not include ancillary items.
				A separate, neckstrap more suitable for long-term carry shall be provided as ancillary equipment (Threshold).
				The CLRF IC full system weight shall be no more than 11.0 lbs (Threshold) and includes those items listed in the above 3.0 lb threshold/2.75 lb objective weight requirement plus the following: remote fire cable, two additional battery cartridges with batteries (of the type which meets the battery life requirements in paragraph 3.15.6), external power cable, azimuth and elevation adjustable Picatinny rail grabber, tripod, tripod soft carry pouch, CLRF IC field carry pouch, eyecup, neckstrap and quick reference card. The following required elements of the CLRF IC system do not count against either of the two weight requirements listed above in this paragraph: transit case, TLDHS cable, GPS crypto fill cable, World Magnetic Model update cable, JTAC LTD cable, Picatinny Rail with mounting hardware and tool(s), Operator’s Manual, and 3 battery cartridges of the other required battery type which is not designated as the primary battery.
			4.9.2	The ability of the CLRF IC to conform to the requirements specified in 3.2 shall be verified through examination. The allowed measurement tolerance is 1% of the required value.
Optics, 3.3	Optical System, 3.3.1	Viewing Optics	3.3.1.1	The CLRF IC shall be monocular (Threshold);
				biocular (Objective).
			4.10.1	The ability of the CLRF IC to conform to the requirements specified in 3.3.1 shall be verified through examination.
		Viewing Sensor	3.3.1.2	It is desired that the CLRF IC will provide direct view optics (Objective).
			4.10.1	The ability of the CLRF IC to conform to the requirements specified in 3.3.1 shall be verified through examination.
	Daytime Target Recognition		3.3.2	The CLRF IC shall permit an operator who is trained in target recognition to be able to recognize an unobstructed, uncamouflaged, 2.1 x 2.1 meter target (oblique angle view of a Toyota Hilux pickup) on a light haze visibility day from 100 meters to 3,000 meters (Threshold);
				100 meters to 4,000 meters (Objective).
			4.10.2.1	The ability of the CLRF IC to conform to the requirements specified in 3.3.2 shall be verified through analysis.
	Nighttime Target Recognition		3.3.3	The CLRF IC shall permit an operator who is trained in target recognition to recognize an unobstructed, uncamouflaged, 2.1 x 2.1 meter target (oblique angle view of a Toyota Hilux pickup) on a light haze visibility night with ¼ moon illumination from 100 meters to 900 meters (Threshold);
				100 meters to 1,500 meters (Objective).
				The CLRF IC shall permit an operator who is trained in target recognition to recognize an unobstructed, uncamouflaged, 2.1 x 2.1 meter target (oblique angle view of a Toyota Hilux pickup) on an overcast starlight night from 100 meters to 900 meters (Objective).
			4.10.2.2	The ability of the CLRF IC to conform to the requirements specified in 3.3.3 shall be verified through analysis.
	Field of View, 3.3.4	Wide Field of View	3.3.4.1	The CLRF IC shall have a wide Field of View (FOV) of at least 120 mils diagonal (Threshold),
				or at least 150 mils (Objective).
			4.10.3	The ability of the CLRF IC to conform to the requirements specified in 3.3.4 shall be verified through examination.
		Narrow Field of View	3.3.4.2	It is desired that a separate narrower field of view not be necessary to meet the target recognition requirements (3.3.2, 3.3.3) (Objective).
				If a separate narrow FOV is required to meet the target recognition requirements (3.3.2, 3.3.3), it shall be no less than 60 mils diagonal (Threshold).
				Additional and/or continuous zoom is desired to allow improved recognition (Objective).
			4.10.3	The ability of the CLRF IC to conform to the requirements specified in 3.3.4 shall be verified through examination.
Angle Measurement Capabilities, 3.4	Azimuth Performance, 3.4.1	Limited Availability Azimuth Measurement	3.4.1.1	The CLRF IC shall measure the Observer to Target (OT) direction with an accuracy of 10 mils or less one sigma, relative to true north, with at least 50% availability in the presence of static, dynamic, and transient magnetic disturbances in 7 seconds or less 90% of the time, and within 9 seconds or less 95% of the time (Threshold).
				The CLRF IC shall measure the OT direction with an accuracy of 8 mils or less one sigma, relative to magnetic north, in a magnetically sterile environment 100% of the time in 2 seconds or less (Threshold).
				Sensor pre-calibration, if required, shall last the duration of the battery life (Threshold), and is not included in this timing requirement.
			4.11.1.1	The ability of the CLRF IC to conform to the requirements specified in 3.4.1.1 between ± 64⁰ latitude shall be verified through demonstration and analysis.
		Full Availability Azimuth Measurement	3.4.1.2	It is desired the CLRF IC measure the OT direction with an accuracy of 10 mils or less one sigma, relative to true north, with 100% availability in the presence of static, dynamic and transient magnetic disturbances in 120 seconds or less (Objective).
				Sensor pre-calibration, if required, shall last the duration of the battery life (Threshold), and is not included in this timing requirement.
			4.11.1.2	The ability of the CLRF IC to conform to the requirements specified in 3.4.1.2 between ± 64⁰ latitude shall be verified through demonstration and analysis.
		Disturbed Magnetic Environment	3.4.1.3	It is desired that the CLRF IC alert the user when the accuracy of the Digital Magnetic Compass exceeds 8 mils (Objective).
			4.11.1.3	The ability of the CLRF IC to conform to the requirements specified in 3.4.1.3 between ± 64 degrees latitude shall be verified through test and demonstration.
	Maintaining Azimuth Upon Relocation		3.4.2	It is desired that the CLRF IC be able to provide the OT direction with an accuracy of 10 mils or less one sigma, relative to true north, for up to 5 minutes after acquiring a true north vector and without re-acquiring a new true north vector. During the 5 minute timeframe the user may reposition and/or change orientation of the device not to exceed a slew rate of 300⁰ per second. (Objective).
			4.11.2	The ability of the CLRF IC to conform to the requirements specified in 3.4.2 shall be verified through demonstration and analysis.
	Vertical Angle		3.4.3	The CLRF IC shall determine the vertical angle (VA) from the observer to a target, through a range of ± 800 mils (Threshold),
				with an accuracy of ± 5 mils one sigma (Threshold)
				to ± 2.5 mils one sigma (Objective).
			4.11.3	The ability of the CLRF IC to conform to the requirements specified in 3.4.3 shall be verified through demonstration.
	Roll Angle		3.4.4	The CLRF IC shall be capable of meeting all operational requirements through roll angles ranging from ± 250 mils (Threshold),
				± 500 mils (Objective).
			4.11.4	The ability of the CLRF IC to conform to the requirements specified in 3.4.4 shall be verified through demonstration.
	Azimuth Upgradeability		3.4.5	It is desired that the CLRF IC provide power, data, and timing lines for a potential future external azimuth system (Objective).
				It is desired that the data line include the following messages per IS-GPS-153, Revision D, Message ID 5029, pages B-86 and B-87 from the azimuth sensor to the CLRF IC: Azimuth Heading, Azimuth Measurement Timestamp, Estimated Azimuth Accuracy, Roll Angle, Roll Angle Accuracy, Vertical Angle, and Vertical Angle Accuracy (Objective).
				It is desired that the data line include the following messages from the CLRF IC to the azimuth sensor: Measurement Request, GPS Location In, Timing Signal, and Azimuth In (when available) (Objective).
				Additional input and output messages, required for communication, may be created as necessary and will follow IS-GPS-153, Revision D format. A draft Interface Control Document (ICD) for the Azimuth and Inertial MEMS (AIM) Future Naval Capability (FNC) program is available from the CLRF IC Contracting Officer. The company which is awarded a CLRF IC LRIP/Production contract will be put in touch with the AIM FNC Principle Investigator to provide input towards finalizing this draft ICD. The ICD will provide more details of the mechanical and electrical interface to, and power requirements of, this potential future external azimuth capability. If this Objective capability is provided, the power draw of the external azimuth capability will not count against the battery life requirements of this Performance Specification.
			4.11.5	The ability of the CLRF IC to conform to the requirements specified in 3.4.5 shall be verified through examination.
Setup Time, 3.5	Rapid Startup Time		3.5.1	The CLRF IC rapid startup shall commence at initiation of power on and complete when the visual displays are up and the operator may begin observation. The CLRF IC shall permit the operator to complete rapid startup in no more than 15 seconds (Threshold);
				less than 5 seconds (Objective).
			4.12.1	The ability of the CLRF IC to conform to the requirements specified in 3.5.1 shall be verified through demonstration.
	Full Setup Time		3.5.2	Full setup shall include all actions necessary for the CLRF IC to provide target location (OT distance, direction, and vertical angle) to the threshold limits, including performing a DMC compensation. With current GPS almanac data, the CLRF IC shall permit the operator to complete full setup in 5 minutes (Threshold);
				2 minutes (Objective).
			4.12.2	The ability of the CLRF IC to conform to the requirements specified in 3.5.2 shall be verified through demonstration.
SAASM GPS, 3.6	SAASM GPS		3.6	The CLRF IC shall include a GPS JPO approved per GPU-09-105 and GPU-09-071 internal SAASM GPS to provide self-location (Threshold).
				The user shall be able to update the DoD World Magnetic Model (WMM) loaded into the SAASM GPS receiver (Threshold). The DoD World Magnetic Model is published by the National Geophysical Data Center (NGDC) of the National Oceanic and Atmospheric Administration (NOAA).
				The GPS receiver shall be capable of operating in either continuous mode or time averaging (Threshold).
				Continuous mode will be the system default setting, and the default setting at system power up (Threshold).
				The CLRF IC shall alert the user whenever self-location or calculated target location is based upon any mode other than continuous (Threshold).
				The CLRF-IC will automatically reset a time-averaging GPS self-location if the system is moved (Objective).
				The user shall be able to load GPS keys, zeroize GPS keys, and check the version of which GPS keys are loaded (Threshold).
			4.13	The ability of the CLRF IC to conform to the requirements specified in 3.6 shall be verified through examination and demonstration.
	Self-Location		3.6.1	The CLRF IC system performing a cold start with the addition of a current almanac for the operating location, shall provide self-location within 70 seconds, 95% of the time (Threshold).
				All classified GPS information and algorithms shall be within the security boundary of the SAASM (Threshold) in accordance with GPU-09-105.
				It is desired that the user be able to manually enter self-location into the CLRF IC (Objective).
			4.13.1	The ability of the CLRF IC to conform to the requirements specified in 3.6.1 shall be verified through analysis, examination, and demonstration.
Laser Rangefinder, 3.7	LRF Eye‑Safety		3.7.1	The CLRF IC shall include a Class 1 eye-safe laser range finder (Threshold).
			4.14.1	The ability of the CLRF IC to conform to the requirements specified in 3.7.1 shall be verified through test and examination.
	Man-Size Target Range Finding		3.7.2	On a 7 km visibility day, the CLRF IC shall measure the distance to a 2.0 m x 0.5 m dismounted man-size target with 50% reflectivity from 100 meters to 2,500 meters (Threshold);
				100 meters to at least 5,000 meters (Objective).
			4.14.2.1	The ability of the CLRF IC to conform to the requirements specified in 3.7.2 shall be verified through demonstration and analysis.
	NATO Standard Target Range Finding		3.7.3	On a 7 km visibility day, the CLRF IC shall measure the distance to a 2.3 meter x 2.3 meter NATO standard target with 10% reflectivity from 100 meters to 4,000 meters (Threshold);
				100 meters to 10,000 meters (Objective).
			4.14.2.2	The ability of the CLRF IC to conform to the requirements specified in 3.7.3 shall be verified through demonstration and analysis.
	Stabilization Device		3.7.4	On a 7 km visibility day, the CLRF IC shall be able to measure the distance to a 2.0 meter x 0.5 meter dismounted man-size target with 50% reflectivity out to at least 2,000 meters without requiring the operator to use a tripod 50 percent of the time (Threshold).
				It is desired that the CLRF IC be able to measure all elements of target location: OT Distance (Requirements 3.7.2, 3.7.3), direction (Requirements 3.4.1.1, 3.4.1.2), VA (Requirement 3.4.3) to the threshold accuracies, without requiring the operator to use a tripod 100 percent of the time (Objective).
			4.14.3	The ability of the CLRF IC to conform to the requirements specified in 3.7.4 shall be verified through demonstration.
	First/Strongest/Last Return		3.7.5	After a single range measurement, the CLRF IC rangefinder shall provide a distance measurement for up to three objects; these three objects shall be the closest, the farthest, and the object with the strongest laser rangefunder (LRF) return(s) between the closest and farthest objects (Threshold).
				If multiple objects are detected, the distances (up to three: closest, strongest in between, farthest) shall be displayed in order from closest to farthest (Threshold).
			4.14.4	The ability of the CLRF IC to conform to the requirements specified in 3.7.5 shall be verified through demonstration.
	Multiple Target Indicator		3.7.6	The CLRF IC rangefinder shall provide a Multiple Target Indicator, which will alert the user in the case that multiple range targets were present during any single range finding operation and allow the user to cycle through and select a desired range (Threshold).
			4.14.5	The ability of the CLRF IC to conform to the requirements specified in 3.7.6 shall be verified through demonstration.
	Range Gate		3.7.7	The CLRF IC shall be equipped with a minimum and maximum range control that permits the operator to set the minimum and maximum range to the nearest 100 meters from 100 meters to the maximum range of the rangefinder, at which the CLRF IC will register a laser return (Threshold). If a system is able to accurately range at distances less than 100 meters, the minimum range gate may be set at that distance vice 100 meters.
				The system shall enable a user to perform this operation in less than 10 seconds (Threshold).
			4.14.6	The ability of the CLRF IC to conform to the requirements specified in 3.7.7 shall be verified through demonstration.
	Glint Protection		3.7.8	The CLRF IC shall provide glint protection in the form of anti-reflective lens coatings (Threshold).
				It is desired that the CLRF IC provide an additional measure of glint protection (Objective). If an additional measure of glint protection is provided, it may be detachable and provided as ancillary equipment which does not count against the system weight requirement. If an additional measure of glint protection is provided, and if it is detachable, then day/night target recognition ranges and laser rangefinding ranges will not be evaluated with the additional measure of glint protection installed.
			4.14.7	The ability of the CLRF IC to conform to the requirements specified in 3.7.8 shall be verified through examination.
	Laser Rangefinder Accuracy		3.7.9	The laser rangefinder shall be accurate to ± 5 meters at one sigma (Threshold).
			4.14.8	The ability of the CLRF IC to conform to the requirements specified in 3.7.9 shall be verified through analysis and/or testing.
	Laser Rangefinder Target Discrimination		3.7.10	The CLRF IC laser rangefinder shall be able to discriminate between two targets separated by 25 meters along the Observer to Target line (Threshold).
			4.14.9	The ability of the CLRF IC to conform to the requirements specified in 3.7.10 shall be verified through analysis and/or testing.
	Laser Rangefinder Probability of Detection		3.7.11	The CLRF IC shall exhibit no more than one range failure out of any 100 consecutive range attempts (Threshold).
			4.14.10	The ability of the CLRF IC to conform to the requirements specified in 3.7.11 shall be verified through demonstration and/or testing.
Laser Spot Imaging, 3.8	1064nm Laser Viewing/ Detection		3.8.1	It is desired that the CLRF IC be capable of viewing or indicating the location of the 1064 nm designator energy within the internal base optic (Objective).
			4.15.1	The ability of the CLRF IC to conform to the requirements specified in 3.8.1 shall be verified through demonstration.
	Reserved		3.8.2
			4.15.2
	IR Pointer Viewing		3.8.3	It is desired the CLRF IC be capable of viewing or indicating the location of 805-870 nm laser energy within the internal base optic (Objective).
			4.15.3	The ability of the CLRF IC to conform to the requirements specified in 3.8.3 shall be verified through demonstration.
	LRF Viewing/ Detection		3.8.4	It is desired that the CLRF IC be capable of viewing or indicating the location of its own rangefinder laser energy within the internal base optic (Objective).
			4.15.4	The ability of the CLRF IC to conform to the requirements specified in 3.8.4 shall be verified through demonstration.
Mechanical Interface, 3.9	Interface with External Devices		3.9.1	The CLRF IC shall interface and operate with the following external devices: Joint Terminal Attack Controller Laser Target Designator (JTAC LTD), AN/PAS-22 Long Range Thermal Imager (LRTI), AN/PAS-25 Thermal Laser Spot Imager (TLSI), and AN/PAS-28 Medium Range Thermal Bi-ocular (MRTB) (Threshold).
			4.16.1	The ability of the CLRF IC to conform to the requirements specified in 3.9.1 shall be verified through examination and demonstration.
	Picatinny Rail		3.9.2	The CLRF IC shall include at least one Picatinny rail provided as ancillary equipment which can mount without any special tools to facilitate mounting day/night sighting optics/imagers (Threshold).
				Any required tool and fasteners, to include threadlocking compound if necessary, shall be provided (Threshold).
				The rail shall be aligned with the emitted laser beams (Threshold).
			4.16.2	The ability of the CLRF IC to conform to the requirements specified in 3.9.2 shall be verified through examination.
	1/4-20 Adapter		3.9.3	The CLRF IC shall have the ability to mount to a standard 1/4-20 UNC threaded tripod (Threshold).
				The 1/4-20 UNC threaded hole shall be integrated into the device on the bottom near the center of gravity (Threshold).
			4.16.3	The ability of the CLRF IC to conform to the requirements specified in 3.9.3 shall be verified through examination.
	Picatinny Rail Grabber		3.9.4	A Picatinny rail grabber shall be provided (Threshold).
				The rail grabber shall be aligned with the optical path of the emitted lasers (Threshold).
				The rail grabber shall contain azimuth and elevation adjustments to facilitate boresighting to a device with a Picatinny rail (Threshold).
				The rail grabber shall be provided as an ancillary equipment adapter that mounts to the CLRF IC without tools (Threshold),
				or it may be integrated into the device (Objective).
				If the rail grabber is provided as an ancillary equipment adapter that mounts to the CLRF IC without tools, re-compensation of the Digital Magnetic Companss (DMC) may be required when the rail grabber is attached or detached from the CLRF IC. Regardless of whether the rail grabber is provided as a separate ancillary equipment adapter or integrated into the device, movement of the azimuth and elevation adjustments shall not require a re-compensation of the DMC in order to comply with the azimuth accuracy requirements (Threshold).
			4.16.4	The ability of the CLRF IC to conform to the requirements specified in 3.9.4 shall be verified through examination.
	Protective Optics Covers		3.9.5	The CLRF IC shall include tethered or hinged covers to protect all lenses (objective, celestial, and eyepiece) and fully block all emitted laser beams (Threshold).
			4.16.5	The ability of the CLRF IC to conform to the requirements specified in 3.9.5 shall be verified through examination and demonstration.
	Carrying Strap and Neck Strap		3.9.6	The CLRF IC shall be equipped with a carrying strap and neckstrap that permits the operator, dressed in all authorized variations of Marine Corps combat clothing, to carry and operate the CLRF IC while it is suspended from his neck (Threshold).
			4.16.6	The ability of the CLRF IC to conform to the requirements specified in 3.9.6 shall be verified through examination.
	Transit Case		3.9.7	The transit case shall be designed to protect the CLRF IC, and associated equipment, from dust, rain, snow, sleet, and salt spray while it is being transported or stored, and be made of a non-reflective material. The transit case shall be able to hold one CLRF IC with carrying strap, neckstrap, tripod, two sets of spare battery packs, associated cables, cleaning kit, ancillary equipment, and operator’s manual (Threshold).
			4.16.7	The ability of the CLRF IC to conform to the requirements specified in 3.9.7 shall be verified through examination.
	Remote Fire Cable		3.9.8	The remote fire cable shall fire upon button release, shall not exceed 1 m in length, and shall trigger a full measurement to calculate a target location within the system (Threshold).
				The remote fire cable shall be able to be used in any system configuration, such as when the CLRF IC is cabled to another device as specified elsewhere in this performance specification (Threshold).
			4.16.8	The ability of the CLRF IC to conform to the requirements specified in 3.9.8 shall be verified through examination and demonstration.
Digital Interface, 3.10	Digital Interface		3.10	When prompted by the operator, the CLRF IC shall output a 5029 serial communication message per IS-GPS-153 Revision D, Message ID 5029, pages B-86 and B-87 (Threshold).
				The 5029 message shall be received by the TLSI and AN/PSQ-19B/C TLDHS (Threshold).
				The CLRF IC shall receive and display information from the JTAC LTD per the Kollsman Documents EI 8388-1000-00 and EICD48081000-1 (Threshold).
				The CLRF IC shall be able to output a 5029 serial message to the AN/PSQ-19B/C TLDHS at all times, regardless of what other equipment it is connected to (Threshold). The CLRF IC does not need to communicate with the TLSI and JTAC LTD simultaneously.
			4.17	The ability of the CLRF IC to conform to the requirements specified in 3.10 shall be verified through demonstration.
	Self-Location Export		3.10.1	It is desired that the CLRF IC output self-location and Figure of Merit information to AN/PSQ-19B/C TLDHS at 1 Hz in accordance with IS-GPS-153 Revision D Message ID 5040 (Objective).
				If this Objective is met, the user shall be able to turn this capability on and off as necessary (Threshold).
				If provided, it is desired that the information outputted in the 5040 message include latitude, longitude, elevation, Estimated Horizontal Error, Estimated Vertical Error, and Estimated Position Error (Objective).
				It is desired that the CLRF IC output a 5040 message following each 5029 message that is generated containing the self-location position at the time the laser was fired which generated the information in the 5029 message (Objective). If these Objective capabilities are provided, they will not count against the battery life requirements of this Performance Specification.
			4.17.1	The ability of the CLRF IC to conform to the requirements specified in 3.10.1 shall be verified through demonstration and analysis.
Interface Cables, 3.11	Interface Cables		3.11	The CLRF IC shall include a AN/PSQ-19B/C TLDHS interface cable (15 pin) per Ashbury Document, Interface Control Document for Vector 21 Modification B-CLRF 2213-A-4005, Rev. 3 which shall be at least 1.5 m in length to permit the operator to connect the CLRF IC to the AN/PSQ-19B/C TLDHS when the operator is holding the CLRF IC in the standing off-hand position and the AN/PSQ-19B/C TLDHS is resting on the ground (Threshold).
				The CLRF IC shall include a JTAC LTD and TLSI interface cable(s) (Threshold).
				The CLRF IC shall include all cables necessary to meet the requirements of this performance specification (Threshold).
			4.18	The ability of the CLRF IC to conform to the requirements specified in 3.11 shall be verified through examination and demonstration.
	Power for Wireless Adapter		3.11.1	It is desired that the CLRF IC serial connector which outputs the 5029 message (and, Objectively, the 5040 message), provide +5 VDC and 500 mA to provide power for a potential future wireless adapter (Objective).
				If this Objective capability is provided, then all requirements of paragraph 3.10.1 Self Location Export, both Threshold and Objective, shall be met (Threshold). If this Objective capability is provided, it will not count against the battery life requirements of this Performance Specification.
			4.18.1	The ability of the CLRF IC to conform to the requirements specified in 3.11.1 shall be verified through analysis, examination, and demonstration
Field Carry Pouch			3.12	A soft material, field carry pouch shall be provided which provides protection against shock and vibration and is attachable to the Modular Lightweight Load-carrying Equipment (MOLLE system (Threshold).
				The field carry pouch shall fit the CLRF IC and two extra sets of batteries inside the field carry pouch or the two extra set of batteries shall fit in an outside compartment on the Field Carry Pouch (Threshold).
				The field carry pouch shall retain the CLRF IC securely to the Marine's body/equipment while walking, running, and jumping and the dimensions of the field carry pouch shall not exceed 1.0 inch more than the maximum length, width, and height of the CLRF IC itself not including an outside compartment on the Field Carry Pouch for the two extra sets of batteries if included. (Threshold).
			4.19	The ability of the CLRF IC to conform to the requirements specified in 3.12 shall be verified through examination and demonstration.
Tripod Soft Carry Pouch			3.13	A soft material, field carry pouch shall be provided to carry the tripod which is attachable to the MOLLE system (Threshold).
				It shall also be able to carry any cables and adapters that are provided with the system which do not fit in the Field Carry Pouch (Threshold).
			4.20	The ability of the CLRF IC to conform to the requirements specified in 3.13 shall be verified through examination and demonstration.
Trigonometric Capabilities			3.14	The CLRF IC shall calculate and display the following trigonometric capabilities: slant range, elevation angle, fall of shot correction, horizontal distance and height difference to remote object, slant range between two remote objects, horizontal and vertical distance between two remote objects, combined azimuth and elevation angle, azimuth and horizontal distance between two remote objects, relative horizontal and vertical angle between two remote objects (Threshold).
			4.21	The ability of the CLRF IC to conform to the requirements specified in 3.14 shall be verified through demonstration.
Battery Compartment, 3.15	Interchangeable Battery Cartridges		3.15.1	The CLRF IC shall be capable of using both CR123 and AA batteries with interchangeable cartridges (Threshold).
				One type of cartridge shall accept AA (lithium or alkaline) and one type of cartridge shall accept CR123s (Threshold).
				It is desired that a single battery cartridge accept both CR123s and AA size batteries (Objective).
				It is desired that the batteries may be inserted into the battery cartridge in any orientation and still function correctly (Objective).
				The battery cartridge shall not be able to be inserted into the system incorrectly (Threshold).
			4.22.1	The ability of the CLRF IC to conform to the requirements specified in 3.15.1 shall be verified through examination.
	Rechargeable Battery Pack		3.15.2	It is desired that, in addition to the use of AA and CR123s, a rechargeable battery be provided and fit the same space as the AA and CR123 cartridges (Objective).
				If a rechargeable battery is provided, it shall not be able to be inserted into the system incorrectly (Threshold).
				If a rechargeable battery is provided, it shall be able to be recharged in the system while connected to external power when the system is both on and off without additional user interaction (i.e. choosing battery type in a menu) (Threshold).
				If a rechargeable battery pack is provided, it is desired that a separate battery charger be provided (Objective).
			4.22.2	The ability of the CLRF IC to conform to the requirements specified in 3.15.2 shall be verified through examination.
	External Power		3.15.3	The CLRF IC shall accept external power from a BA-5590 and BB-2590 (Threshold).
			4.22.3	The ability of the CLRF IC to conform to the requirements specified in 3.15.3 shall be verified through demonstration.
	System Damage		3.15.4	The CLRF IC shall not be damaged by over/under voltage from external power sources. The system shall not be damaged by connecting or disconnecting to the external battery while the system is operating (Threshold).
			4.22.4	The ability of the CLRF IC to conform to the requirements specified in 3.15.4 shall be verified through demonstration
	Battery Status		3.15.5	The CLRF IC system shall provide a low power battery status indicator that alerts the user when the CLRF IC has only enough battery life remaining for 30 +/- 15 minutes of operation (Threshold).
			4.22.5	The ability of the CLRF IC to conform to the requirements specified in 3.15.5 shall be verified through examination.
	Battery Life		3.15.6	The CLRF IC shall permit 6 hours of operation on one of the following types of batteries: either a single set of CR123 or a single set of AA batteries (Threshold).
				It is desired that the CLRF IC will permit 8 hours of operation on a single set of CR123 or AA batteries (Objective).
				If the CLRF IC is unable to meet these battery life requirements for the nominal mission profile defined in paragraph 3.1 with the GPS receiver always on in continuous mode, then the user shall be able to select a minimum of two modes; GPS always on and GPS power conservation (Threshold).
				In always on mode the GPS receiver shall operate in continuous mode and remain on unless positively turned off by the user, even if the rest of the system enters an automatic standby or sleep mode (Threshold).
				In power conservation mode the SAASM GPS receiver shall enter sleep mode with a time set by the user (Threshold).
				The battery life requirements shall be met with a sleep mode time out of no less than 5 minutes (Threshold),
				or while the GPS receiver is in the always-on mode (Objective).
			4.22.6	The ability of the CLRF IC to conform to the requirements specified in 3.15.6 shall be verified through demonstration.
	Auto Power Shut-Off		3.15.7	The CLRF IC shall execute an auto-shutdown command to automatically turn off the system after 20 minutes without operator interaction (Threshold).
			4.22.7	The ability of the CLRF IC to conform to the requirements specified in 3.15.7 shall be verified through demonstration.
Boresight Alignment			3.16	The system shall maintain internal boresight across all FOVs, magnifications, optical systems, lasers and laser receivers to within 0.5 mils over the operational temperature range (Threshold).
				It is desired the CLRF IC not need boresight adjustments after delivery (Objective).
			4.23	The ability of the CLRF IC to conform to the requirements specified in 3.16 throughout the operating temperatures shall be verified through examination.
Tripod			3.17	The tripod shall be non-reflective, non-magnetic, weigh less than or equal to 2.5 lbs, have a course and fine adjustment capability for azimuth and elevation, and be at least equal in durability to the CLRF IC (Threshold).
				It is desired to weigh less than or equal to 2.0 lbs (Objective).
			4.24	The ability of the CLRF IC to conform to the requirements specified in 3.17 shall be verified through examination. If this capability is met through the combination of the Picatinny Rail Grabber of 3.9.4 and a tripod with course adjustment capability, then the full tripod weight shall be the combined weight of both the tripod and the Picatinny Rail Grabber.
Tripod Size			3.18	The tripod shall be compact enough, when not in use, to fit in the cargo pocket of the standard issue camouflage utility uniform (Threshold).
				The tripod shall be adjustable from 10-22 inches in height (Threshold).
				It is desired that the lower height adjustment range extend down to 8 inches (Objective).
				It is desired that the upper height adjustment range extend up to 34 inches (Objective).
			4.25	The ability of the CLRF IC to conform to the requirements specified in 3.18 shall be verified through examination.
Viewing Optics, 3.19	Eye Protection		3.19.1	The CLRF IC optics shall contain Laser Eye Protection capable of, at a minimum, attenuating laser radiation levels below the Class I AEL at the aperture for an 80 mJ energy 1064 nm laser and an 860 nm 1 Watt power IR Pointer laser (Threshold).
			4.26.1	The ability of the CLRF IC to conform to the requirements specified in 3.19.1 shall be verified through examination.
	Eyepiece, 3.19.2	Diopter Adjustments	3.19.2.1	The CLRF IC optics shall have a diopter adjustment from +2 to -6 diopters (Threshold).
			4.26.2.1	The ability of the CLRF IC to conform to the requirements specified in 3.19.2.1 shall be verified through examination.
		Exit Pupil	3.19.2.2	The CLRF IC optics shall have an exit pupil diameter not less than 6mm (Threshold).
			4.26.2.2	The ability of the CLRF IC to conform to the requirements specified in 3.19.2.2 shall be verified through examination.
		Eye Relief	3.19.2.3	The CLRF IC optics shall have an eye relief not less than 18mm (Threshold).
			4.26.2.3	The ability of the CLRF IC to conform to the requirements specified in 3.19.2.3 shall be verified through examination.
	Reticle and Reticle Scales, 3.19.3	Reticle Operation	3.19.3.1	The CLRF IC reticle shall be viewable by the operator during daylight and nighttime operation (Threshold).
			4.26.3.1	The ability of the CLRF IC to conform to the requirements specified in 3.19.3.1 shall be verified through demonstration.
		Reticle Resolution	3.19.3.2	The CLRF IC reticle shall be graduated in 5 mil increments and labeled in 10 mil increments (Threshold).
			4.26.3.2	The ability of the CLRF IC to conform to the requirements specified in 3.19.3.2 shall be verified through examination.
		Reticle Pattern	3.19.3.3	The CLRF IC reticle shall be of a mil-scale variety (as shown in Figure 3‑1) to allow trained users to estimate ranges (Threshold),
				user-selectable (Objective).
			4.26.3.3	The ability of the CLRF IC to conform to the requirements specified in 3.19.3.3 shall be verified through examination.
	Data Display		3.19.4	The CLRF IC system shall simultaneously display target location data (OT True Azimuth, OT Range, OT Vertical Angle), 10-digit grid target location, 10-digit grid self-location, and shall include indication of coordinate reference, measurement units, battery status, multiple returns, north reference, and an indication when a Figure of Merit (FOM) 2 or better accuracy is not achieved within the eyepiece (Threshold).
			4.26.4	The ability of the CLRF IC to conform to the requirements specified in 3.19.4 shall be verified through demonstration.
	Legibility, 3.19.5	Visibility	3.19.5.1	The CLRF IC system visual display shall be legible under all light conditions encountered during system operation even when users are wearing polarized eye wear (Threshold).
				CLRF IC display shall have a user-selectable light level down to fully off for night (Threshold).
			4.26.5.1	The ability of the CLRF IC to conform to the requirements specified in 3.19.5.1 shall be verified through demonstration.
		Display Viewing	3.19.5.2	The CLRF IC display shall be viewable to the user without removing his eye from the eyepiece (Threshold).
			4.26.5.2	The ability of the CLRF IC to conform to the requirements specified in 3.19.5.2 shall be verified through examination.
		Visual Display Features	3.19.5.3	The CLRF IC shall display the Data Display (3.19.4) within 2 seconds of completion of measurement (Threshold).
				If the CLRF IC visual display of targeting data has a timeout feature, it shall have a user selectable time (Threshold).
			4.26.5.3	The ability of the CLRF IC to conform to the requirements specified in 3.19.5.3 shall be verified through demonstration.
	Display Units		3.19.6	The CLRF IC shall display angle measurements in mils and degrees and be user selectable (Threshold).
				The CLRF IC shall display the north reference in user-selectable grid, true, or magnetic (Threshold).
				The CLRF IC system shall display ranges in meters or yards (user-selectable) in single digit increments (Threshold).
				The CLRF IC shall display self-location and target location in user-selected coordinate format per IS-GPS-153, Revision D (Threshold).
				The CLRF IC shall display FOM (Threshold).
			4.26.6	The ability of the CLRF IC to conform to the requirements specified in 3.19.6 shall be verified through demonstration.
	Display Precision, 3.19.7	Precision of Data Display	3.19.7.1	The CLRF IC system data display precision shall be less than or equal to 1 mil when set to mil units or less than or equal to 0.1⁰ when set to degrees (Threshold).
			4.26.7.1	The ability of the CLRF IC to conform to the requirements specified in 3.19.7.1 shall be verified through examination.
		Precision of Digital Data	3.19.7.2	The CLRF IC digital data precision for angular measurements shall be less than or equal to 0.1 mil (Threshold).
				The CLRF IC digital data precision for distance shall be less than or equal to 0.1 m (Threshold).
			4.26.7.2	The ability of the CLRF IC to conform to the requirements specified in 3.19.7.2 shall be verified through demonstration.
	Target Location Error Indicator, 3.19.8		3.19.8	It is desired that the CLRF IC system display an estimation of the Target Location Error (TLE) in meters (dictated by the Joint Close Air Support publication 3-09.3, dated 08 July 2009) to the user for each measurement taken and include the errors introduced from self-location accuracy, range finding accuracy, and azimuth accuracy (Objective).
				The corresponding TLE Category may also be displayed, but the TLE Category shall not be displayed without the TLE in meters (Threshold). TLE Categories are shown in Figure 3‑2.
			4.26.8	The ability of the CLRF IC to conform to the requirements specified in 3.19.8 shall be verified through demonstration.
	Safety Messages, 3.19.9	Warning Messages	3.19.9.1	The CLRF IC shall display a warning message notifying the user that their present position is less than the user-defined Minimum Safe Range value from the target position and injury or death could result (Threshold).
			4.26.9.1	The ability of the CLRF IC to conform to the requirements specified in 3.19.9.1 shall be verified through demonstration.
		Danger Messages	3.19.9.2	The CLRF IC shall display a danger message notifying the user that their present position to the target location is less than 100 m from the target position used and injury or death could result (Threshold).
				The Warning Message and Danger Message are mutually exclusive. If both conditions are met, only the Danger Message will be displayed (Threshold).
			4.26.9.2	The ability of the CLRF IC to conform to the requirements specified in 3.19.9.2 shall be verified through demonstration.
Built-in-Test (BIT), 3.20	BIT Accuracy		3.20.1	The CLRF IC shall have a BIT capability that will check system status with 95% accuracy (Threshold).
				It is desired the BIT capability have 99% accuracy (Objective).
			4.27.1	The ability of the CLRF IC to conform to the requirements specified in 3.20.1 shall be verified through demonstration and analysis.
	BIT False Alarm Rate		3.20.2	The false alarm rate shall be less than 10% for system status tests (Threshold).
			4.27.2	The ability of the CLRF IC to conform to the requirements specified in 3.20.2 shall be verified through demonstration and analysis.
	BIT Display		3.20.3	The CLRF IC system BIT capability shall display the software version and check the display (Threshold).
			4.27.3	The ability of the CLRF IC to conform to the requirements specified in 3.20.3 shall be verified through demonstration.
Graceful Degradation, 3.21			3.21	CLRF IC shall be designed for graceful degradation, meaning that the failure of one or more subsystems shall not result in the failure of the entire system, and, in as much as is practicable, shall not compromise the mission (Threshold).
			4.28	The ability of the CLRF IC to conform to the requirements specified in 3.21 shall be verified through analysis.
System Signature, 3.22	Aural Detectability		3.22.1	It is desired that the CLRF IC aural detectability distance be less than 20 meters during operation (Objective).
			4.29.1	The ability of the CLRF IC to conform to the requirements specified in 3.22.1 shall be verified through testing in accordance with requirement 2, Table 2-II of MIL-STD-1474D.
	Stray Light Security		3.22.2	A method shall be provided that allows the operator to adjust the brightness of all illuminated indicators to minimize detection (Threshold).
				If the eyecup used is a self-closing eye cup, it shall be able to be locked in the open position once fully depressed, or shall be tethered and able to be readily removed and replaced without tools (Threshold).
				It is desired that the CLRF IC not be visible (displays, indicators) at ranges greater than 20 meters to unaided viewing or when viewing with 3rd generation NVGs (Objective).
			4.29.2	The ability of the CLRF IC to conform to the requirements specified in 3.22.2 shall be verified through demonstration.
Environmental Requirements, 3.23	Chemical, Biological, Radiological and Nuclear (CBRN) Decontamination		3.23.1	The CLRF IC shall be able to withstand, with limited operational degradation, at least 4 exposures to the material-damaging effects of CBRN contaminants, decontaminants, and decontaminating procedures in a 72-hour period (Threshold),
				indefinitely (Objective). NOTE: Removing and discarding external covering materials to meet this requirement is acceptable provided the procedure to do so can be performed by the operator in a tactical environment and that the functionality of the CLRF IC is not degraded by the removal of the covering material. MIL-HDBK-783 and MIL-HDBK-784 may be referred to for guidance.
			4.30.1	The ability of the CLRF IC to conform to the requirements specified in 3.23.1 shall be verified through analysis.
	Military Free Fall Operations-Altitude (Non‑Operational)		3.23.2	The CLRF IC shall not suffer any damage or degradation in performance (as a result of atmospheric pressure related effects) after being subjected to a military free fall operation while being carried by a user conducted from 25,000 ft Mean Sea Level (MSL) (Threshold).
				It is desired that The CLRF IC will not suffer any damage or degradation in performance (as a result of atmospheric pressure related effects) after being subjected to a military free fall operation conducted from 42,000 ft MSL (Objective).
			4.30.2	To determine conformance to 3.23.2, the CLRF IC shall be tested for atmospheric pressure related effects at altitude. Altitude testing shall be in its transit case at 7,620 m (25,000 ft) Mean Sea Level (MSL) at an altitude change rate of 8 m/s to 10 m/s (26 ft/s to 33 ft/s) for a period of 1 hour within the operating temperatures specified in 3.23.7 in accordance with MIL-STD-810G, Method 500.5, Procedure I.
	Reserved		3.23.3
			4.30.3
	Immersion (30 ft)		3.23.4	The CLRF IC shall not suffer any damage or degradation in performance following a 30‑minute submersion in water at a depth of 30 ft while sealed in a waterproof bag (Threshold).
				It is desired that the CLRF IC will not suffer any damage or degradation in performance following a 30‑minute submersion in water at a depth of 50 ft while sealed in a waterproof bag (Objective).
			4.30.4	To determine conformance to 3.23.4, the CLRF IC shall be tested in accordance with MIL-STD-810G, Method 512.5, Procedure I. The system shall be conditioned for 2 hours at 50⁰F above the water temperature.
	Immersion (1.0 meter)		3.23.5	The CLRF IC shall not suffer any damage or degradation in performance following a 10 minute submersion unprotected in fresh or salt water at a depth of 1.0 m (Threshold).
			4.30.5	To determine conformance to 3.23.5, the CLRF IC shall be tested in accordance with MIL-STD-810G, Method 512.5, Procedure I. The system shall be conditioned for 2 hours at 50⁰F above the water temperature.
	Humidity		3.23.6	The CLRF IC shall not suffer any damage or degradation in performance between 0% and 100% humidity (Threshold).
			4.30.6	To determine conformance to 3.23.6, the CLRF IC shall be tested in accordance with MIL-STD-810G, Method 507.5, Procedure 2, for 10 cycles per Figure 507.5-7.
	Operating Temperature		3.23.7	The CLRF IC shall be capable of operating in air temperatures ranging from -25⁰F to 125⁰F (Threshold).
			4.30.7	To determine conformance to 3.23.7, the CLRF IC shall be tested in accordance with MIL-STD-810G, Method 501.5, Procedure II (high temperature), and Method 502.5, Procedure II (low temperature). The system shall soak at 60 minutes at each temperature.
	Storage Temperature		3.23.8	The CLRF IC shall be capable of being stored in temperatures ranging from -30⁰F to 145⁰F without the benefit of the field carry pouch or transit case (Threshold).
			4.30.8	To determine conformance to 3.23.8, the CLRF IC shall be tested in accordance with MIL-STD-810G, Method 501.5, Procedure I (high temperature), and Method 502.5, Procedure I (low temperature). The system shall soak at 60 minutes at each temperature. The system shall not be in its field carry pouch or transit case while being tested.
	Temperature Shock		3.23.9	The CLRF IC shall not suffer any damage or degradation in performance following sudden changes in ambient air temperature of up to 35.6⁰F/min (Threshold),
				or up to 50⁰F/min (Objective).
			4.30.9	To determine conformance to 3.23.9, the CLRF IC shall be tested in accordance with MIL-STD-810G, Method 503.5, Procedure I-B, between ambient air temperatures of -14°F and 122°F for a period of two (2) hours at each temperature.
	Fungus		3.23.10	The CLRF IC (free of all salt residues) shall neither support fungal growth nor suffer damage or degradation of performance caused by the presence of fungus spores or adjacent fungal growth (Threshold).
			4.30.10	The ability of the CLRF IC to conform to the requirements specified in 3.23.10 shall be analyzed in accordance with MIL-STD-810G, Method 508.6.
	Mechanical Vibration (Minimum Integrity)		3.23.11	The CLRF IC, within its transit case, shall be able to withstand the vibration effects experienced during transport in military aircraft (to include helicopter), cross-country (off-road) vehicular movement, and maritime transport (Threshold).
			4.30.11	To determine conformance to 3.23.11, the CLRF IC shall be tested in accordance with MIL-STD-810G, Method 514.6, Procedure I General Vibration. Random vibration levels shall be as identified in Figure 514.6E-1 of Annex E (General Minimum Integrity Exposure), with a test duration of one hour for each of three orthogonal axes. Inspect for damage and verify system operation after completion of testing.
	Transport Vibration (Loose Cargo)		3.23.12	While in its transit case, the CLRF IC shall operate without damage or degradation following exposure to transportation vibration (Threshold).
			4.30.12	To determine conformance to 3.23.12, the CLRF IC shall be tested in accordance with MIL-STD-810G, Method 514.6, Procedure II, Category 5 (Threshold). The total test time shall be three hours.

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