Attachment 0004 - XM919 IAM P-Spec Compliance Matrix.xlsx
XLSX spreadsheet 35 KB Posted
- Solicitation number
- W15QKN-23-R-0056
About this file
This document is a compliance matrix for an Individual Assault Munition (IAM) system specification. It outlines over 100 performance, design, safety, and testing requirements for an XM919 IAM to be procured by the Department of the Army Materiel Command Contracting Command Picatinny Arsenal. Key requirements include defeating 30mm armor at 200m, incapacitating structures at angles from 0-30 degrees, withstanding various environmental and transportation tests, and having over 90% reliability. Offerors must provide test data and citations to show where their proposal addresses each requirement in the compliance matrix. The solicitation number and opportunity details are also provided.
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Compliance Matrix1
| No | Requirement Catagory | Sub-Catagory | Requirement Paragraph | Performance Specification Requirement Paragraph | Testing Standard | Minimum Test Quantity* | Notes: | Proposal Refernece Data Location (Pg/Section/Para) |
| 1 | Performance Lethality /Range | Anti-Armor | 3.4.6.1 | Armor. The XM919 warhead given a single shot shall defeat a stationary or moving, fully exposed vehicle with not less than 30 millimeters of Rolled Homogeneous Armor (RHA) constructed in accordance with MIL-DTL-12560 using 30-second assault criteria at a 0° obliquity angle of at 200 meters. | ITOP 2-2-716, |
ITOP 4-2-812A Performance Testing Of Shaped Charge Warheads 4 rounds moving 200m/max range
| 5 rounds /PTSCW | Armor Penetration verification IAW para 4.4.6.1 conducted IAW ITOP 4-2-812A. Dynamic testing shall be conducted using a semi-infinite RHA target set at 0° obliquity, 200 meters from the muzzle, in accordance with MIL-DTL-12560. Use depth/feeler gauge or x-ray radiography to determine depth of penetration. Minimum required demonstration of defeat is defined as penetration at or beyond 30mm. Full testing of armor defeat (defeat will encompass damage to the vehicle (mobility (M-kill), firepower (F-kill), or mobility and firepower (M or F-kill)) or expected fractional casualties (30-second assault criteria) to other than crew, mounted occupants (Fc)) is required during PVT | ||||||
| 2 | Performance Lethality /Range | Anti-Structure | 3.4.6.3 | Building. The XM919 warhead given a single shot shall incapacitate a randomly located, crouching, protected Soldier within: a sixteen-inch adobe structure; a double reinforced eight-inch concrete wall; and a brick/concrete masonry unit (CMU) structure; constructed in accordance with ITOP 5-2-503 and ITOP 5-2-518, using 30-second defense casualty criterion, at an angle of 0° to 30° (adobe structure at 0° only) at 200 meters. | ITOP 05-2-503 and ITOP 05-2-518, | 3 rounds at 0°, 200m/max range | |
| 3 rounds at 30°, 200m/max range | Dynamic testing shall be conducted with a target set at 0° obliquity and 30° obliquity at 200m range. Double Reinforced Concrete (DRC) targets shall be constructed in accordance with ITOP 05-2-503 Appendix E paragraph 3.4 at eight-inch thickness. Adobe targets shall be constructed in accordance with ITOP 05-2-503 Appendix E paragraph 3.2 at sixteen-inch thickness (testing conducted at 0° obliquity only). Brick/CMU target shall be constructed in accordance with ITOP 05-2-503; the brick compressive strength shall be between 3.5 and 6 ksi. All target structures shall be constructed in accordance with ITOP 05-2-518. Defeat is defined as penetration of and detonation behind the target wall. | ||||||
| 3 | Performance Lethality /Range | Field Fortifications | 3.4.6.2 | Bunker. The XM919 warhead given a single shot shall defeat the sidewall or roof or incapacitate occupants of an earth and timber bunker, constructed in accordance with ITOP 5-2-503, using 30-second defense casualty criterion at an angle of 0° to 30° at 200 meters. | ITOP 05-2-503 | 3 rounds at 0°, 200m/max range | |
| 3 rounds at 30°, 200m/max range | Dynamic testing shall be conducted with a target set at 0° obliquity and 30° obliquity at 200m range. Earth & Timber Bunker (E&TB) targets shall be constructed in accordance with ITOP 05-2-503A ITOP 05-2-503 Appendix E paragraph 3.5. Minimum required demonstration of defeat is defined as penetration of and detonation behind the target wall. Full testing of bunker defeat (the collapse (defeat) the sidewall or roof of an earth and timber bunker and/or achieve a fractional casualty (Fc) of the bunker occupants using 30-second defense casualty criterion) is required during PVT. | ||||||
| 4 | Performance Lethality /Range | Range | 3.4.3 | Range. |
a. The XM919 shall have a minimum engagement range not greater than 30 meters.
| b. The XM919 shall have a maximum engagement range not less than 200 meters. | 5 rounds at 200m or maximum range | |||||
| 5 | Performance | Fire From Enclosure | 3.4.8 | Fire From Enclosure (FFE) The XM919, when operator fired from within an enclosed room (1260 cubic feet volume – 12’x15’x7’) with two openings (window and door) either in the kneeling or standing position shall be safe to the operator wearing double hearing protection . The operator shall be able to fire a minimum of one or more rounds over a 24-hour period (MIL-STD-1474). See 3.5.8 (Acoustic Energy) for additional details. | ITOP 05-2-517A | |
| MIL-STD-1474 | 5 rounds hot conditions |
5 rounds ambient conditions 5 rounds cold conditions
| 6 | Performance Lethality /Range | Maximum Arming Distance | 3.5.10.1.2 | Maximum arming distance. The maximum fuze arming distance shall not be greater than 30 meters. | JOTP-10B | No Minimum quantity of test rounds |
| 7 | Lethality /Accuracy | Accuracy | 3.4.5 | Accuracy. |
a. The XM919’s accuracy when measuring the distance from the aimpoint to the hit point shall have a standard deviation no greater than or equal to 0.5 meters in height and width at a distance of 200 meters for a sample size of 10 rounds throughout the operating temperature range.
b. All target impacts shall be within a 4 meter by 4 meter area around a central aim point at a distance of 200 meters throughout the operating temperature range. ITOP 4-2-829 10 rounds hot conditions 10 rounds ambient conditions 10 rounds cold conditions
| 8 | Lethality /Accuracy | Probability of Hit | 3.4.4.1 | Stationary target. The XM919, when operator fired at a stationary 2.3 meter by 2.3 meter target not less than 200 meters away, shall achieve a probability of hit of not less than 0.6. | ITOP 4-2-829 | No Minimum quantity of test rounds |
| 9 | Lethality /Accuracy | Probability of Hit | 3.4.4.2 | Moving target. The XM919, when operator fired at a 2.3-meter (height) by 4.6-meter (length) target moving at 15 kilometers per hour, in a direction perpendicular to the line of fire, not less than 200 meters away, shall achieve a probability of hit of not less than 0.4. | ITOP 4-2-829 | No Minimum quantity of test rounds |
| 10 | Performance Reliability | Logistics/storage | 3.5.15.4 | Storage temperature. The XM919 shall meet all safety and performance requirements when used in the operating environment after being stored at a temperature of: |
a. Not less than constant -46°C (-50°F) for not less than 72 hours and
b. Not greater than two-hour at +71°C (+160°F) during diurnal cycle high temperature exposure for a minimum of 7 cycles JOTP-10B 5 rounds constant 5 rounds diurnal
| 11 | Performance Reliability | Environmental Extremes | 3.7.1 | Air jump. The XM919 shall be capable of air-jump (static line and military free fall) with an individual parachutist and meet the safety and performance requirements following air-jump. | JOTP-10B | N/A -Will be evaluated post Award |
| 12 | Performance Reliability | Environmental Extremes | 3.7.7 | Operating temperature. The XM919 shall meet all safety and performance requirements when operated between -40°C plus or minus 3°C (-40°F plus or minus 5.4°F) also referred as cold temperature and +60°C plus or minus 3°C (+140°F plus or minus 5.4°F) also referred as high temperature. Unless noted otherwise the requirements in the specification shall be applicable throughout the operating temperature range. (See 6.19.32 for operating/storage temperature definitions). | 10 rounds | |
| 13 | Performance Reliability | Ruggedness | 3.7.5.1.1 | Logistic wheeled vehicle transportation dynamics. The XM919 shall be capable of withstanding logistical wheeled vehicle transportation dynamics per JOTP-010 without impact to safety and performance. | JOTP-10B | |
| 14 | Performance Reliability | Ruggedness | 3.7.5.1.2 | Packaged transit drop. The packaged XM919 shall not fire, arm, or be partially armed upon impact when dropped 2.1 meters per JOTP-010 and meet all safety and performance requirements. | JOTP-10B | |
| 15 | Performance Reliability | Ruggedness | 3.7.2 | Air drop. The XM919 shall be capable of resupply by air-dropped bundles and meet the safety and performance requirements following air drop. | JOTP-10B | N/A -Will be evaluated post Award |
| 16 | Performance Reliability | Ruggedness | 3.7.5.2.1 | Military wheeled vehicle transportation vibration (dynamics). The XM919 shall not fire, arm, or be partially armed during military wheeled vehicle transportation dynamics (vibration) per JOTP-010 and meet all safety and performance requirements. | JOTP-10B | 10 rounds |
| 17 | Performance Reliability | Ruggedness | 3.7.5.2.2 | Restrained cargo transport shocks. The XM919 shall not fire, arm, or be partially armed during restrained cargo transport shocks per JOTP-010 and meet all safety and performance requirements. | JOTP-10B | 10 rounds |
| 18 | Performance Reliability | Ruggedness | 3.7.5.2.3 | Loose cargo repetitive shock. The XM919 shall not fire, arm, or be partially armed during loose cargo repetitive shock per JOTP-010 and meet all safety and performance requirements. | JOTP-10B | 10 rounds |
| 19 | Performance Reliability | Ruggedness | 3.7.5.3.1 | Helicopter cargo transportation vibration. The XM919 shall not fire, arm, or be partially armed during helicopter cargo transportation vibration per JOTP-010 and meet all safety and performance requirements. | JOTP-10B | 10 rounds |
| 20 | Performance Reliability | Ruggedness | 3.7.6.3 | Air transport dynamics. The XM919 shall not fire, arm, or be partially armed during air transport dynamics per JOTP-10 and meet all safety and performance requirements. | JOTP-10B | 10 rounds |
| 21 | Performance Reliability | Ruggedness | 3.7.6.4 | Land transport dynamics. The XM919 shall not fire, arm, or be partially armed during military land transportation dynamics per JOTP-10 and meet all safety and performance requirements. | JOTP-10B | 10 rounds |
| 22 | Performance Reliability | Ruggedness | 3.7.5.4 | Tactical drop/impact. The unpackaged XM919 shall not fire, arm, or be partially armed upon impact when dropped 1.5 meters per JOTP-010 and meet all safety and performance requirements. | JOTP-10B | 10 rounds |
| 23 | Performance Reliability | Ruggedness | 3.7.5.5 | 12-meter logistic drop. The XM919 shall remain safe to handle and dispose of following a drop from 12-meters per JOTP-010. The XM919 shall not discharge or become armed or partially armed. | JOTP-10B | 3 rounds (1 per orientation) |
| 24 | Performance Reliability | Ruggedness | 3.7.5.6 | Induced loading. . The XM919 shall be capable of withstanding an induced load of 113kg, intending to simulate a Soldier in full battle gear either sitting or falling on the item and meet all safety and performance requirements. | 2 rounds | |
| 25 | Performance Reliability | Environmental Extremes | 3.7.6.1 | Salt fog. The XM919 shall be capable of withstanding exposure to salt fog per JOTP-010, without impact to safety and performance, specifically no evidence of corrosion, deterioration of exterior, or clogging/binding. | JOTP-10B | 2 rounds |
| 26 | Performance Reliability | Environmental Extremes | 3.7.6.9 | Ice/freezing rain. |
a. The XM919 shall be capable of exposure to ice/freezing rain per JOTP-010 without impact to safety and performance.
b. The XM919 shall be capable of deicing after exposure to ice/freezing rain.
| c. The XM919 shall be fully operational and effective in an icy/freezing rain environment. | JOTP-10B | 2 rounds | |||||
| 27 | Performance Reliability | Environmental Extremes | 3.7.6.10 | Mud. The XM919 shall be capable of withstanding mud immersion per TOP 03-2-045 without impact to safety and performance. | TOP 3-2-045 | 2 rounds | |
| 28 | Performance Reliability | Environmental Extremes | 3.7.6.2 | Sand and dust. |
a. The XM919 shall be capable of withstanding exposure to sand and dust per JOTP-010, without impact to safety and performance.
| b. The XM919 shall be fully operational and effective in a sandy and/or dusty environment. | JOTP-10B | 2 rounds | |||
| 29 | Performance Reliability | Environmental Extremes | 3.7.6.3 | Humidity. |
a. The XM919 shall be capable of withstanding exposure to high and low humidity in high and low temperature environments per JOTP-010 without impact to safety and performance.
| b. The XM919 shall be fully operational and effective in a high, normal, and low humidity environment. | JOTP-10B | 10 rounds | |||
| 30 | Performance Reliability | Environmental Extremes | 3.7.6.4 | Water immersion. |
a. The XM919 shall be capable of withstanding fresh water immersion per JOTP-010 without impact to safety and performance.
| b. The XM919 shall be fully operational and effective in a wet/rainy environment. | JOTP-10B | 2 rounds | |||||
| 31 | Performance Reliability | Environmental Extremes | 3.7.6.5 | Temperature cycle. The XM919 shall be capable of withstanding temperature cycling per JOTP-010 without impact to safety and performance. | JOTP-10B | 10 rounds | |
| 32 | Performance Reliability | Environmental Extremes | 3.7.6.6 | Thermal shock. The XM919 shall be capable of withstanding thermal shock per JOTP-010 without impact to safety and performance. | JOTP-10B | 10 rounds | |
| 33 | Performance Reliability | Environmental Extremes | 3.7.6.7 | Solar radiation. The XM919 shall be capable of withstanding solar radiation per JOTP-010 without impact to safety and performance. | JOTP-10B | 2 rounds | |
| 34 | Performance Reliability | Environmental Extremes | 3.7.6.8 | Altitude decompression. The XM919 shall be capable of withstanding rapid decompression per JOTP-010 without impact to safety and performance. | JOTP-10B | 2 rounds | |
| 35 | Performance Reliability | Climatic Conditions | 3.7.9.9 | Fungus. |
a. The XM919 shall be capable of exposure to fungus per JOTP-10 without impact to safety and performance.
| b. The XM919 shall be capable of decontamination after exposure to fungus. | JOTP-10B | 2 rounds | |||||
| 36 | Performance Reliability | Logistics/storage. | 3.5.15.2 | Shelf life. The XM919 shall remain safe, operable, and meet all requirements of this specification within its operating temperature range (see 3.7.7) after not less than five (5) years of uncontrolled storage (see 6.19.31) and after not less than twenty (20) years of controlled storage without maintenance other than periodic surveillance, packaging, and preservation per TB 9-1300-385 and DA PAM 742-1. | TB 9-1300-385 and SB 742-1 | 18 rounds | |
| 37 | Performance Reliability | Reliability | 3.4.1 | Reliability. The XM919 shall have an overall reliability value of not less than 0.91. | 18 rounds | ||
| 38 | Performance Reliability | Reliability | 3.4.2 | Production reliability. The XM919 shall have a production reliability value of not less than 0.91 or better. | 18 rounds | ||
| 39 | Performance Reliability | Logistics/storage. | 3.5.15.3 | Field life. The XM919 shall remain safe, operable, and meet all requirements of this specification within its operating temperature range (see 3.7.7) after not less than 1 year of field handling while removed from its packaging. Field life consists of exposure to environments listed in section 3.7. | 18 rounds | ||
| 40 | Portability | System Length | 3.6.1 | Length. The XM919’s length in the carry configuration, including the carry case, if applicable, shall not exceed 106.7 centimeters (42 inches). | 5 rounds | ||
| 41 | Portability | System Weight | 3.6.2 | Weight. The XM919 shall include an adjustable quick release carry strap that can support the weight of the XM919 and does not interfere with its operation. | 5 rounds | ||
| 42 | Design | Carry Strap | 3.6.10 | Carry strap. The XM919 shall include an adjustable quick release carry strap that can support the weight of the XM919 and does not interfere with its operation. | No Minimum quantity of test rounds | ||
| 43 | Design | Markings | 3.5.16.1 | Warnings. The XM919 shall have clearly marked safety warnings and a diagram of the back blast area in English. | No Minimum quantity of test rounds | ||
| 44 | Design | Markings | 3.5.16.2 | Identification. The XM919 and its parts, components, and subassemblies shall be marked for identification in accordance with MIL-STD-130 and MIL-STD-1168. Each round shall be legibly marked with national stock number (NSN), LOT number and serial number. | MIL-STD-130 and MIL-STD-1168. | No Minimum quantity of test rounds | |
| 45 | Design | Markings | 3.5.16.3 | Instructions. The XM919 shall have clearly marked and simple-to-follow step-by-step firing instructions in English | No Minimum quantity of test rounds | ||
| 46 | Design | Markings | 3.5.16.4 | Adhesives. All markings, identifications, and instructions that utilize adhesive(s) shall use adhesives durable under the environments specified in paragraph 3.7. | No Minimum quantity of test rounds | ||
| 47 | Design | Markings | 3.5.15.1 | Lot numbering. Ammunition lot numbering and serialization for all XM919 units shall be in accordance with MIL-STD-1168. | MIL-STD-1168. | No Minimum quantity of test rounds | |
| 48 | Design | Markings | 3.5.16.5.1 | Ammunition. The XM919’s ammunition shall be color-coded and marked in accordance with MIL-STD-709. | MIL-STD-709. | No Minimum quantity of test rounds | |
| 49 | Design | Non-Dedicated Gunner | 3.6.12 | Simple to operate. The XM919 shall be able to be operated without any specialized training (see 6.19.19 and 6.19.29). | No Minimum quantity of test rounds | ||
| 50 | Design | Non-Dedicated Gunner | 3.6.13 | Non-dedicated gunner. The XM919 shall be operable by one operator and not require a dedicated gunner. | No Minimum quantity of test rounds | ||
| 51 | Design | Non-Dedicated Gunner | 3.6.4 | Preparation for firing. The XM919 shall be capable of being prepared by hand (no tools needed) for firing in accordance with the affixed firing instructions, safety warnings, and the operator’s manual. | No Minimum quantity of test rounds | ||
| 52 | Design | Non-Dedicated Gunner | 3.6.5 | One-handed oepration. While holding with one hand and shouldering the XM919, the operator shall be able to use the other hand to perform all necessary weapon functions. | No Minimum quantity of test rounds | ||
| 53 | Design | Safety and Selector | 3.5.6 | Safety selector switch. The XM919 shall have a safety selector switch (see Table I, VI, VII Critical Characteristics) with the following features: | |||
| a. | Provide unambiguous tactile and visual indications that it is fully armed or non-armed. | ||||||
| b. | Safety selector switch shall remain in the designated position, either safe or armed, as required by the operator. | ||||||
| c. | Indicator failure shall not result in a false non-armed condition indication. | ||||||
| d. | In the non-armed condition, the color of the lettering background shall be Brown Semi-Gloss, per SAE-AMS-STD-595/20150, with the letter “S” or the word “SAFE” superimposed thereon in Miscellaneous Gloss (white), per SAE-AMS-STD-595/17875 or per SAE-AMS-STD-595/17925. Alternatively, if the launcher is colored Olive drab then the lettering background shall be Green Gloss per SAE-AMS-STD-595/14187. | ||||||
| e. | In the armed condition, the color of the lettering background shall be Brown Semi-Gloss, per SAE-AMS-STD-595/20150, with the letter “A” or the word “ARMED” superimposed thereon in Miscellaneous Gloss (white), per SAE-AMS-STD-595/17875 or SAE-AMS-STD-595/17925. Alternatively, if the launcher is colored Olive drab then the lettering background shall be Green Gloss per SAE-AMS-STD-595/14187. | ||||||
| f. | Font size shall be legible during limited visibility (rain, fog, after dusk). | ||||||
| g. | Colors shall be nonspecular. | No Minimum quantity of test rounds | |||||
| 54 | Design | Compatibility | 3.6.8.1 | Sight. At a minimum the XM919 shall have a standard militarized sight (see 6.19.15). | No Minimum quantity of test rounds | ||
| 55 | Design | Compatibility | 3.6.8.2 | Sight power source. If required, the sight shall utilize a commercial off-the shelf commonly available battery. | No Minimum quantity of test rounds | ||
| 56 | Design | Compatibility | 3.6.8.3 | Sight interface.The XM919 shall be capable of interfacing with existing individual night vision devices (including night sights and aiming lights). | No Minimum quantity of test rounds | ||
| 57 | Design | Compatibility | 3.6.9 | Attachment rails. The XM919 shall have one US Army standard interface rails, per MIL-STD-1913, that: |
a. shall be an integral part of each item,
b. shall provide a means for mounting, without tools, all of the night sighting devices,
c. shall not be attachable or removable, and
| d. shall not be collinear. | No Minimum quantity of test rounds | |||||
| 58 | Design | Compatibility | 3.6.16 | Free of protrusions. The XM919, in the carry configuration, shall be free of protrusions which would become entangled during maneuvers. | No Minimum quantity of test rounds | |
| 59 | Design | Compatibility | 3.6.17 | Terrain. The XM919, in the carry configuration, shall be portable by the operator over varying difficult terrain and for long distances. | No Minimum quantity of test rounds | |
| 60 | Design | Compatibility | 3.6.18 | Balanced load. The XM919, in the carry configuration, shall have a method(s) of carry which will provide a balanced load for the operator. | No Minimum quantity of test rounds | |
| 61 | Design | Compatibility | 3.6.7.1 | Equipment compatibility. The XM919 shall be able to be carried and employed in all operational conditions and compatible with existing combat, cold weather, and personal equipment, including Mission Oriented Protective Posture (MOPP) gear. | No Minimum quantity of test rounds | |
| 62 | Design | Compatibility | 3.6.7.2 | Soldier compatibility. The XM919 shall be able to be carried and employed in all operational conditions, to include airborne, air assault, and waterborne operations. | No Minimum quantity of test rounds | |
| 63 | Design | Compatibility | 3.6.14 | Time to fire. The XM919 shall require no greater than 19 seconds to bring from the carry configuration to the standing, ready-to-fire configuration. | No Minimum quantity of test rounds | |
| 64 | Design | Compatibility | 3.6.11.1 | Operation. The XM919’s trigger assembly shall require a continuous force not less than 10 Newtons and not greater than 50 Newtons to operate. | No Minimum quantity of test rounds | |
| 65 | Design | Compatibility | 3.6.11.2 | Unobstructed sight. The XM919’s trigger assembly shall not obstruct the operator’s sight picture during trigger activation. | No Minimum quantity of test rounds | |
| 66 | Design | Logistics/storage. | 3.5.15.6 | Demilitarization. |
a. The XM919 shall be capable of demilitarization in a manner that the military offensive or defensive advantages are eliminated to prevent further use for the originally intended military or lethal purpose, explosive hazards are eliminated, and by-products of the demilitarization process are disposed in compliance with environmental regulations and in accordance with DoDI 5000.02 5.d.(14)(b)2, DoD 4160.21-M, and DoDI 4140.62 (see 6.5).
| b. The XM919 design shall enable all energetic components to be disassembled from the munition and segregated for disposition with minimal labor and in a cost-effective manner. | DoDI 5000.02 5.d.(14)(b)2, DoD 4160.21-M, and DoDI 4140.62 | No Minimum quantity of test rounds | |||||
| 67 | Design | Markings | 3.5.16.5.2 | Overall exterior. The XM919’s overall exterior shall be colored in accordance with SAE-AMS-STD-595/30145 (no less than 90%) Butternut Stain, or alternately SAE-AMS-STD-595/34088 (no less than 90%) Olive Drab and color-coded in accordance with MIL-STD-709. | SAE-AMS-STD-595/34088 & MIL-STD-709 | No Minimum quantity of test rounds | |
| 68 | Design | Markings | 3.5.17 | Workmanship. The external surface of the XM919 shall be in accordance with manufacturer’s standard as submitted during design verification test. The surface shall be clean, marked legibly, and free of chips, dirt, grease, rust and foreign material. The external surface shall be free of burrs and sharp edges, which may affect performance or result in injury during handling. | No Minimum quantity of test rounds | ||
| 69 | Design | Interface and interoperability requirements. | 3.6.15 | Disposable. The XM919 shall be a disposable, self-contained, one-shot system. | No Minimum quantity of test rounds | ||
| 70 | Design | Interface and interoperability requirements | 3.6.6 | Function time. The elapsed time from when the trigger is depressed, and the projectile is completely free of the barrel shall be not greater than 200 milliseconds. (see Table VI, Critical Characteristics) | |||
| 5 rounds | |||||||
| 71 | Safety | E3 | 3.7.3 | Electromagnetic Environmental Effects (E3) The XM919 shall comply with DoD policies on E3 in accordance with MIL-STD-461, MIL-STD-464, and MIL-STD-1316. | |||
| JOTP-10B | |||||||
| MIL-STD-461, MIL-STD-464, and MIL-STD-1316. | No minimum quantity but proof of testing/certification is required | ||||||
| 72 | Safety | E3 | 3.7.3.1 | Hazard of electromagnetic radiation to ordnance (HERO). The XM919 shall remain safe after exposure to HERO. | JOTP-10B | No minimum quantity but proof of testing/certification is required | |
| 73 | Safety | E3 | 3.7.3.2 | Electrostatic discharge (ESD). The XM919 shall remain functional and safe per requirements in JOTP-062 in the following configuration: | JOTP-10B | No minimum quantity but proof of testing/certification is required | |
| 74 | Safety | E3 | 3.7.3.2.1 | Personal electrostatic discharge (PESD). The XM919 shall remain functional and safe for transportation, storage, handling and firing after exposure in its unpackaged configuration to PESD | JOTP-10B | No minimum quantity but proof of testing/certification is required | |
| 75 | Safety | E3 | 3.7.3.2.2 | Helicopter electrostatic discharge (HESD). The XM919 shall remain functional and safe for transportation, storage, handling and firing after exposure in its unpackaged and packaged configuration to HESD. | JOTP-10B | No minimum quantity but proof of testing/certification is required | |
| 76 | Safety | E3 | 3.7.3.3. | Electromagnetic compatibility (EMC). The XM919 shall be electromagnetically compatible within itself and safely meet all operational performance requirements. Susceptibility tests shall be carried out on the XM919 in accordance with MIL-STD-461 and MIL-STD-464. | MIL-STD-461 and MIL-STD-464. | No minimum quantity but proof of testing/certification is required | |
| 77 | Safety | E3 | 3.7.3.4 | Lightning hazard. The XM919 shall remain functional and safe for transportation, storage, handling and firing after exposure to near strike lightning. The XM919 shall be assessed for safe disposal after exposure to direct strike lightning to assess the safety of the weapon. | JOTP-10B | No minimum quantity but proof of testing/certification is required | |
| 78 | Safety | Insensitive Munitions | 3.5.4 | Insensitive munitions.The XM919, when packaged in accordance with the packaging provisions of the contract, shall be reviewed by the Insensitive Munitions Board (see 6.10). | MIL-STD 2105D | No Minimum quantity of test rounds | |
| 79 | Safety | Compatibility | 3.6.19 | Re-stowage. The XM919 shall be able to be returned to a safe carrying and storage configuration after accomplishing all actions short of firing. | No Minimum quantity of test rounds | ||
| 80 | Safety | System Stability | 3.5.10.1.1 | Safe separation distance. The fuze arming distance shall be not less than the safe separation distance. The safe separation distance shall be determined by modeling data collected during the arena fragmentation test. (see Table I, VI, VII Critical Characteristics). | |||
| 81 | Safety | System Stability | 3.5.10.1.2 | Maximum arming distance. The maximum fuze arming distance shall not be greater than 30 meters. | |||
| 82 | Safety | System Stability | 3.5.10.2 | Army Fuze Safety Review Board (AFSRB) certification. The fuzing design shall be safety certified by the Army Fuze Safety Review Board or by the Joint Services Fuze and Ignition System Safety Authorities (JS-FISSA). Reference AR 385-10 and Army Fuze Safety Review Board (AFSRB) Guidebook. | No Minimum quantity of test rounds | ||
| 83 | Safety | System Stability | 3.5.10.3 | Fuze testing. Fuze level testing shall comply with the requirements of MIL-STD-331 and JOTP-052. | MIL-STD-331D, JOTP-052 | No Minimum quantity of test rounds | |
| 84 | Safety | System Stability | 3.5.10.4 | Fuze safety. Fuze design shall conform to MIL-STD-1316. (see Table VI, Critical Characteristics) | MIL-STD-1316 | No Minimum quantity of test rounds | |
| 85 | Safety | System Stability | 3.5.10.5 | Fuze logic device. Fuze designs that utilize electronic logic devices for safety related functions shall conform to JOTP-051. | JOTP-051 | No Minimum quantity of test rounds | |
| 86 | Safety | System Stability | 3.5.10.6 | Fuze software. Fuze designs that utilize software for safety related functions shall conform to the Army Fuze Safety Review Board (AFSRB) Guidebook, AOP-52, and the Joint Service Software System Safety Handbook. | JOTP-051 | No Minimum quantity of test rounds | |
| 87 | Safety | System Stability | 3.5.11.1 | Energetic material qualification. All energetic materials used in the XM919 shall be qualified for their intended military use by the U.S. Army Qualification Authority or by the U.S. Navy Qualification Authority in accordance with the contract statement of work (see 6.8). | No Minimum quantity of test rounds | ||
| 88 | Safety | System Stability | 3.5.11.2 | Energetic materials compatibility. All energetic materials (i.e., explosives, propellants, pyrotechnics, etc.) utilized shall be compatible with all combinations of directly contacting energetic and non-energetic materials. In addition, they shall be compatible with all combinations of materials that have the potential for contact in the system’s life cycle (i.e., manufacturing environment, storage, etc.). | MIL-STD-650 | No Minimum quantity of test rounds | |
| 89 | Safety | System Stability | 3.5.11.3 | Weight of propellant (Launch safety) - The amount of propellant shall be measured to an accepted weight that will ensure launch safety (see 3.5.3) and function time (3.6.6) and not cause a failure to the toxic fumes/sealing of propellant gases (see 3.5.9). | No Minimum quantity of test rounds | ||
| 90 | Safety | Compatibility | 3.6.21 | Built-in test equipment.If the firing mechanism employs stored electrical energy there shall be built-in test equipment to check that sufficient firing current is available and capable of multiple built-in test cycles. | No Minimum quantity of test rounds | ||
| 91 | Safety | Compatibility | 3.6.7.3 | Chemical compatibility. All materials utilized shall be compatible with all combinations of directly contacting energetic and non-energetic materials. In addition, they shall be compatible with all combinations of materials that have the potential for contact in the system’s life cycle (i.e., manufacturing environment, storage, etc.). | JOTP-10B | No Minimum quantity of test rounds | |
| 92 | Safety | Reliability/ | |||||
| Soldier Safety | 3.4.7 | Projectile flight integrity. The projectile and its associated components shall remain intact and be aerodynamically stable until target impact. (see Table I, VI, VII Critical Characteristics) | Test flight data of all rounds tested. minimum sample size of 23 rounds | ||||
| 93 | Safety | System Stability/ | |||||
| Soldier Safety | 3.5.1 | Unintentional detonation. The XM919, including the fuze, shall not experience unintentional function at any point prior to firing, and at any point from engagement of the trigger through flight to target. (see Table VI, Critical Characteristics) | JOTP-10B | Test flight data of all rounds tested. minimum sample size of 23 rounds | |||
| 94 | Safety | System Stability/ | |||||
| Soldier Safety | 3.5.12.1 | Warehead arena trials. Warhead arena trails tests shall be conducted to collect the spatial distribution of fragments data to determine and confirm safe separation distances and range safety parameters. | No Minimum quantity of test rounds | ||||
| 95 | Safety | System Stability/ | |||||
| Soldier Safety | 3.5.12.2 | Surface danger zone (SDZ). The XM919’s surface danger zone shall not exceed the footprint for existing similar systems as described in DA PAM 385-63 Chapter 6. | No Minimum quantity of test rounds | ||||
| 96 | Safety | System Stability/ | |||||
| Soldier Safety | 3.5.13 | Explosive ordnance disposal (EOD). The XM919 shall be safe to handle, pickup, and transport by EOD personnel after firing or after the application of the EOD render safe procedures (see 6.6). | No Minimum quantity of test rounds | ||||
| 97 | Safety | System Stability/ | |||||
| Soldier Safety | 3.5.14 | Factor of safety (Launcher strength). The XM919 pressure vessel(s) of the launch tube shall have a safety margin of not less than 1.2 for components constructed of metals, and not less than 1.5 for components constructed of composite materials/non-metals (see Table VI, Critical Characteristics). Factor of Safety (FOS) is calculated as stated below for the launch platform and the projectile. For systems that include a rocket motor or additional pressure vessels, it is also required to meet the factor of safety for these items (in addition to the launch platform). |
SF = [B – 3 x Sb]/[C + 3 x Sc] = [B – 3 x Sb]/ MEOP
Where:
B = average of peak burst pressures (demonstrated by test, on production representative samples Sb = standard deviation of the peak burst pressures C = average of propellant peak chamber operating pressures (propellant) at worst case temperature or conditions leading to the highest average operating pressure.
Sc = standard deviation of peak chamber operating pressure (firing at hot temp.)
| MEOP = maximum expected operating pressure = C + 3 x Sc | No minimum quantity but proof of testing required | |||
| 98 | Safety | System Stability/ | ||
| Soldier Safety | 3.5.2 | Safety from debris. No debris resulting from discharge of the XM919 shall cause injury or death to the operator. (see Table I, VI, and VII , Critical Characteristics) | JOTP-10B | 6 rounds hot conditions |
6 rounds cold conditions
| 99 | Safety | System Stability/ | ||
| Soldier Safety | 3.5.3 | Launch safety. The initial propulsion event shall be contained and completed within the launch tube. Subsequent propulsion events, if applicable, shall not cause any hazard to the operator. (see Table I, VI, and VII Critical Characteristics) | 6 rounds hot conditions |
6 rounds cold conditions
| 100 | Safety | System Stability/ | |
| Soldier Safety | 3.5.8 | Acoustic energy. The individual operator, equipped with either single or double hearing protection (see 6.19.29) shall, over a 24 hour period, be capable of firing in the following environment: |
a. Free field environment. In the prone, kneeling, or standing position (see 6.19.9, 6.19.11, 6.19.24, 6.19.30), one or more rounds fired with single hearing protection and two or more rounds fired with double hearing protection.
| b. Fire from enclosure/Confined space (double hearing protection)*. One or more rounds in an enclosure in the kneeling or standing positions, also referenced as fire from enclosure (see 6.19.3). (see Table I, VI, VII Critical Characteristics) | JOTP-10B | 15 rounds confined space (5 rounds @ each temp range) (Db Level recorded @ Gunner Head position while firing) | ||
| 101 | Safety | System Stability/ | ||
| Soldier Safety | 3.5.9 | Toxic fumes. The individual operator shall not be exposed above Occupational Safety and Health Administration (OSHA) Permissible Exposure Levels (PEL) and/or American Conference of Governmental Industrial Hygienists (ACGIH) Threshold Limit Values (TLVs) and ensure launch safety (see 3.5.3) and function time (3.6.6). | JOTP-10B | No Minimum quantity of test rounds |
| 102 | Safety | System Stability/ | ||
| Soldier Safety | 3.6.20 | Forecoil/Recoil. The XM919’s forecoil shall be not greater than 65 Joules in the forward direction and the recoil shall be not greater than 35 Joules in the rearward direction. (see Table VI, Critical Characteristics) . | JOTP-10B | 3 rounds hot conditions |
3 rounds cold conditions
| 103 | Safety | System Stability/ | ||
| Soldier Safety | 3.6.3 | Firing positions. The XM919 shall be able to be fired in the prone, kneeling, modified kneeling, and standing positions (see 6.19.11, 6.19.24, 6.19.30). | 5 rounds prone |
5 rounds kneeling/modified 5 rounds standing
| 104 | Safety | System Stability/ | |
| Transport Safety | 3.5.5 | Final hazard classification (FHC). The XM919 shall comply with the following hazard classification or be less hazardous when packaged in accordance with packaging provisions of the contract or purchase order. |
DOD Hazard Class/Div/SCG: 1.1E DOT Hazard Class: 1.1E
| DOT Label: Explosive 1.1E | TB-700-2 | Submit HC or IHC certification if available OR will be evaluated post Award | |||||
| 105 | Safety | System Stability/ | |||||
| Transport Safety | 3.5.7 | Transportation safety. The XM919 shall have a device (transportation safety) that will prevent initiation of the munition while being transported. The transportation safety shall remain in place until removed by the operator. It shall be independent of the safety selector switch (see 3.5.6) and the fuze (see 3.5.10). (see Table I, VI, VII Critical Characteristics) | No Minimum quantity of test rounds | ||||
| 106 | Maintenance | Maintenance | 3.5.15.5 | Maintenance. The XM919 shall require no planned maintenance other than periodic surveillance, packaging and preservation, and Preventative Maintenance Checks and Services (PMCS) per DA PAM 742-1. | No Minimum quantity of test rounds | ||
| 107 | Survivability | CBRNE Survivability | 3.7.4.1 | CBR decontaminable. In the packaged configuration, the XM919 shall be able to be decontaminated from nuclear, biological, and chemical attacks/environments. | TOP 8-2-111 | No Minimum quantity of test rounds | |
| 108 | Survivability | CBRNE Survivability | 3.7.4.2 | CBR operable. The XM919 shall be operable in an unpackaged configuration in a Nuclear, Biological, and Chemical (NBC) environment. | TOP 8-2-111 | No Minimum quantity of test rounds | |
| * Tests can be combined to minimize required rounds needed to achieve test data/results | |||||||
| NA = Minimum number of rounds Not Appliable however supporting evididence still required to support meeting or exceeding requirement unless specifically stated it will be tested post award e.g. PVT |
Instructions
| No | Requirement Catagory | Sub-Catagory | Paragraph | Performance Specification Requirement Paragraph | Verification Standard | Minimum Test Quantity | Notes: | Proposal Refernece Data Location (Pg/Section/Para) |
| 1 | Performance Lethality /Range | Anti-Armor | 3.4.6.1 | Armor. The XM919 warhead given a single shot shall defeat a stationary or moving fully exposed vehicle with not less than 30 millimeters of Rolled Homogeneous Armor (RHA) constructed in accordance with MIL-DTL-12560 using 30-second assault criteria at a firing angle of 0° at 200 meters. | ITOP 2-2-716, |
ITOP 4-2-812A Performance Testing Of Shaped Charge Warheads 4 rounds moving 200m/max range 5 rounds /PTSCW EXAMPLE: Volume 1: Techcnical; Section 1: Sub-Factor 1: Performance: - Armor pg xx. Test Report dated 1/15/2021 RHA Penetration test; Photo exibit #123; test data sheet (attachment b.)
| INSTRUCTIONS: |
| Enter in column (I) reference to the location(s) where in the proposal volume response the requirement supporting data, test report, table, or photos which substantiate system performance against the system specification. |
All Perfromance Specifications must be addressed
File details come from the government source that posted it. Updated .