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Single base propellants

Sporting ammunition describes rifle and handgun ammunition for hunting and target practice. Commercial hunting bullets, ranging in size from around 6 to 12mm, may differ from the conical shape of military bullets in that they [Pg.9]

Artillery ammunition for guns, howitzers, cannons, and mortars ranges upwards in calibre from the 20mm limit that generally divides it from small-arms ammunition. Artillery ammunition is divided into three types  [Pg.10]

Large-calibre artillery ammunition permits a more complex payload including high explosives, bursters, shrapnel, bursting charges, fuzes, incendiaries, etc. [Pg.10]

In addition to catalysts, stabilizers, opacifiers (to reduce heat radiation ahead of the flame), flash depressants, plasticizers, and binders, the main fuel and oxidizers for rocket propellants include [Pg.11]

While the term missile can apply to any projectile ammunition, guided missiles describes those rockets whose course or trajectory is controlled electronically by computers and communications equipment. [Pg.11]


Pure nitroglycerin is a stable Hquid at temperate conditions. It decomposes above 60°C to form nitric oxides which in turn catalyze further decomposition. Moisture increases the rate of decomposition under these conditions. Double- and multibase propellants containing nitroglycerin have substantially shorter stabiHty Hves at 65 and 80°C than do single-base propellants. The decomposition of nitroglycerin proceeds as... [Pg.12]

Single-base propellants are mixed in a similar fashion by adding the ingredients to the nitrocellulose in the mixer together with the required amounts of ether and alcohol. The mixing time is about one-half hour, and the temperature is kept below 25°C. The pardy colloidal mixture looks like moist cmde sugar. A maceration step may be included to increase homogeneity. [Pg.44]

Continuous Solvent—Extrusion Process. A schematic for a typical continuous process, widely used for making solvent propellant for cannons, is shown in Figure 7. This continuous process produces ca 1100 metric tons of single-base propellant per month at the U.S. Army Ammunition Plant (Radford, Virginia). Continuous processes have also been developed for double- and triple-base propellants and for stick as well as granular geometries. A principal aspect of these processes has been the extensive use of single- and double-screw extmders instead of the presses used in the batch process. [Pg.44]

Fig. 7. Continuous process for solvent-extmded single-base propellant (automated single-base line). Vey = conveyor. Fig. 7. Continuous process for solvent-extmded single-base propellant (automated single-base line). Vey = conveyor.
Single base propellants are basically nitrocellulose which has been made colloidal by the action of solvent. [Pg.169]

Single base propellant. Propellant based on nitrocellulose without the inclusion of nitroglycerine. [Pg.201]

Single-base propellants, 10 725 Single-carbon insertion reactions in organoboranes, 13 654—657 Single-cell drum filters, 11 357 Single-cell protein(s) (SCP), 13 688,16 315, 26 474... [Pg.847]

Single-base propellants are made from NC that is gelatinized with the solvents ethanol or diethyl ether. A small amount of diphenylamine, (C6H )2NH, is also... [Pg.90]

Table 4.8 Physicochemical properties of a single-base propellant. Table 4.8 Physicochemical properties of a single-base propellant.
Of these, the most successful appeared in 1887 when Alfred Nobel patented a nitrocellulose propellant plasticised with nitroglycerine. Known as a double-base propellant, it is virtually smokeless, with a very high specific impulse as compared to gunpowder. Single-base propellants were developed in 1865 and 1890 by Schultz and Vieille respectively and these took the form of gelatinised nitrocellulose for use in firearms and mortars. [Pg.57]

Single Base Propellant. See under Propellants and in Ref 44, p C31-R under CANNON PROPELLANTS... [Pg.752]

A. Polveri alia sola nitrocellulosa a solvente volatile o Polveri a una base (Single Base Propellants with Volatile Solvent). To these belong a proplnt listed by Giorgio, p 205 as Polvere italiana per cartucce cal 8 per mitragliatrice, which contd NC (12.8% N) 97, Centralite 2... [Pg.437]

A) Nitrocellulose or Single-Base Propellants (Shokayaku) contd NC (Nitrocellulose) (ca 12.5% N) 98 DPhA (Diphenylamine) 2%. [Pg.494]

T. Suzuki et al, Small-Arms Single-Base Propellant Charge , USP 3442213 (1969) CA 71,118(1969)... [Pg.514]

Ethanol, Ether and Water Determination in Single-Base Propellants by US Army Munition Command Method T 103.5 entitled Total Volatiles, Gas Chromatographic Method.. The method is described in MIL-STD-2688, 30 June 1971... [Pg.35]

Ethanol -i- Ether, as "Residual Solvent" Determination in Single-Base Propellants (US Ordnance Methods). Determine the percentage of total volatiles (Solvents + Moisture), then of moisture and subtract percentage of moisture from percent of total volatiles to obtain residual solvent... [Pg.37]

For determination of Moisture in single-base propellants, three methods can be used ... [Pg.42]

Uses of Ether. One of the important applications of ether is in manuf of single-base propellants whece it is used in 2 1 mixture (by wt) with ethanol. The procedure is described in Vol 3 of Encycl, p C399, under Colloiding Agents and Colloidal Propellants... [Pg.58]

Single-Base Propellants Double-Base Propellant... [Pg.534]

It was adopted by the US Ordnance Dept (Ref 2), but the temperatures of the test were 120° for double-base propellants and 134.5° for single-base propellants for NC s (Ref 3). Litmus paper was originally used in this test (Refs 1 8c 2) but later this was changed id methyl violet paper and the test was called the Methyl Violet Test Apparatus ... [Pg.712]


See other pages where Single base propellants is mentioned: [Pg.43]    [Pg.44]    [Pg.169]    [Pg.170]    [Pg.187]    [Pg.56]    [Pg.20]    [Pg.89]    [Pg.90]    [Pg.91]    [Pg.127]    [Pg.317]    [Pg.750]    [Pg.786]    [Pg.501]    [Pg.765]    [Pg.89]    [Pg.90]    [Pg.91]    [Pg.127]    [Pg.213]   
See also in sourсe #XX -- [ Pg.169 ]




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Single base propellant composition

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Typical Single-Base Solid Propellants

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