ICS, Doc ID, ITOP Title, Drop Tests for Munitions. Original Title. Category, IS / TS. Location. ITOP Drop Tests for Munitions, Final Report on International Test Operations Procedure. ITOP (2), Safety Testing of Field Artillery Ammunition. – ITOP , Drop Test for Munitions. – ITOP , Rough Handling Tests.

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The maximum external payload capabilities of U. The objective of this sub test is to detennine the suitability of the test item to be transported by U. Compliance with the Energetic materials compatibility requirements shall be validated during the design verification test. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. All weapons shall be loaded to capacity and the test shall be performed until the total test sample quantity is reached.

The average center of impact of the 5 shot groups, fired at ambient temperature, shall not exceed 2 inches from the point of aim at a target 2 meters from the muzzle of the Mossberg Model shotgun. Load maintains directional stability for most maneuvers.

Failure to eject 0 1 Major The objective of this sub test is to determine whether the test item can be transported over and off highways. If a test loading is conducted, describe the measured interferences between the test itpo and the aircraft. The second length dimension is the unobstructed allowable cargo length form front of cargo compartment to transmission box.

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No visible permanent deformation or set in the provisions or supporting structure shall result from the application of the loads. Proper safety regulations will be adhered to when using the test courses.

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Speeds will be determined by specified type of test courses. Upon completion of de-rigging, conduct a visual and functional inspection of the load.

External fire test d. Cartridge length, max Level IV 3. The time that the cartridges are out of temperature for movement between the conditioning chamber and the test cell, as well as the test setup, shall be regained in conditioning at a 1: The cartridges shall be fired from two Mossberg Modelfrom a range of 2 meters and two Remington Modelfrom a range up to 3-inches.

The gross weight equals the gross vehicle weight rating GVWR or the maximum projected weight of the equipment, which ever is greater. The weight and balance center of gravity of the aircraft is vitally important to its stability. The cartridges will then be stored under ambient condition for 48 hours. Aircraft is constantly unstable. The lot shall be rejected if the requirement is not met.

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Prior to load application, secure the equipment to a bedplate, deadman, or some means of attachment for anchoring purposes. Any shock and vibration measurements of internal components or members should be accompanied by comparable recordings at the base of the test item forcing function. Rigging diagrams and procedures. The cartridges shall be function fired from the Mossberg and Remington and the muzzle velocity shall be measured.

Cartridge cases from one unchanged process and from one manufacturer.

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The cartridge lot shall contain: Using the appropriate recovery vehicle, or the vehicle specified in the requirements document, connect the test item to the recovery vehicle with standard towbars to the towing pintle or utop and tie-down provisions per the test item’s technical manual. Ambient 4 0 1 3. When specified see 6. The following documents form a part of this document to the extent specified herein.

Record of test item condition for test fuel and lubricant levels, missing or damaged components.