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Bulk loaded liquid propellants are an artillery technology that was pursued at the U.S. Army Research Laboratory and U.S. Naval Weapons Center from the 1950s through the 1990s. The advantages would be simpler guns and a wider range of tactical and logistic options.
Handgun propellants may reach peak pressure before the bullet leaves the cartridge case, while rifle propellants may move a bullet several inches before reaching peak pressure. [ 4 ] : 125 The motion and behavior characteristics of projectiles while under the influence of the gases produced by the propellant is known as internal ballistics .
The United States Army divides supplies into ten numerically identifiable classes of supply.The North Atlantic Treaty Organization (NATO) uses only the first five, for which NATO allies have agreed to share a common nomenclature with each other based on a NATO Standardization Agreement (STANAG).
Number 4831 was used to load navy anti-aircraft machine gun ammunition, and number 4895 was used to load United States service rifle ammunition. As these propellants became military surplus after the war, large quantities of different batches were blended together to make products with uniform average performance for sale to civilians.
The primary mission of the RFAAP is to manufacture propellants and explosives in support of field artillery, air defense, tank, missile, aircraft, and naval weapons systems. As of 2011 RFAAP is operated by BAE Systems under contract to the US Army Joint Munitions Command. The current Commander for the Radford Army Ammunition Plant (RAAP) is Lt ...
Firearm propellants (1 C, 19 P) R. Rocket propellants (4 C, 19 P) Pages in category "Propellants" ... Bulk loaded liquid propellants; 1,2,4-Butanetriol trinitrate; C.
Smokeless powders are typically classified as division 1.3 explosives under the UN Recommendations on the Transport of Dangerous Goods – Model Regulations, regional regulations (such as ADR) and national regulations. However, they are used as solid propellants; in normal use, they undergo deflagration rather than detonation.
Used on the Titan I, the LR87-3 burned liquid oxygen and RP-1. [4] Following the retirement of the Titan missile program, these engines saw no further use. [citation needed] The LR87-3 was also operated with NTO/Aerozine 50 and ground tested with LOX/H2 (with a new fuel pump), making it one of very few engines to have been run on three different propellant combinations.
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