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Binders solid rocket propellants

A Small but important daSS of fOi mUlatiOnS comprises the Composite Solid Rocket Propellants. Composites typically contain a major amount of an oxidizer such as AP or HMX, a metal powder such as Al, a binder which is one or another type of rubber (or double-base), and up to a dozen trace ingredients such as catalysts, stabilizers, etc. There are literally hundreds of formulations, all to a degree similar and the choice comes down to specific missions, economics, and special requirements Loading of End Items. The blends and formulations described above may be loaded into their hardware in the plant where they are made, or they may be shipped to another plant for Load/... [Pg.796]

BAMO is perhaps the most prominent among the azido oxetanes class in terms of the number of polymers and copolymers reported so far. Due to its symmetrical azido groups, it assumes special significance as a hard block repeating unit in a thermoplastic elastomer. However, the homopolymer is solid and cannot be used directly for binder applications because of its crystal-tine nature. Also, poly(BAMO) shows relatively poor mechanical properties as a binder for solid rocket propellants [153]. Many copolymers of BAMO with non-energetic co-monomers tike tetrahydrofuran (THF) have been reported. The BAMO-THF copolymer is an excellent candidate for binder applications with its energetic BAMO content coupled with the THF block which affords... [Pg.263]

Kirk Othmer 11 (1953), 777 stated that AN can be used as an oxidizer in rocket propellants in place of K perchlorate V)Warren (1958), p 1 lists a solid rocket propellant consisting of AN 80, elastomeric binder 18 additives 2%. He also discusses on pp 34-5 the use of AN as an oxidizer in rocket propellants W)Dr L.Deffet, Belgium listed in private communication, 10 March 1954,the following AN expls as currently manufd in Belgium Alkalite, Alsilite, Centralite TA, Cooppalite Dynamite III, Flammivore,... [Pg.353]

Aeroplex Propellants are solid rocket propellants developed and manufd by the Aerojet Engineering Corp, Azusa, Calif. They consist of a finely divided crystalline oxidizer (such as Amm or K perchlorate)dispersed in a thermosetting resin(such as styrene, methyl acrylate, etc), acting as a fuel. In addition there are binders (such as resins) and other ingredients. Aeroplex propellants differ from the usual NC or NC-NG propellants not only in physical and chemical properties, but also in their methods of manuf... [Pg.108]

The objectives of the ongoing work is to explore the chemical synthesis of possible replacements for AP as an oxidizer in tactical missile rocket motors. The synthesis, sensitivities, thermal stability, binder compatibility and decomposition pathways of these new high-oxygen materials are currently being researched. In the following example, we theoretically want to evaluate, the suitability of nitrosyl (N0+) and nitronium (NCB,) oxalate as a potential ingredient for solid rocket propellants. [Pg.126]

Low acrylonitrile) Gaskets, grommets, and O-rings (flexible at a very low temperature), adhesives. Fuel binder in solid rocket propellants. [Pg.892]

Use Gasoline and oil-loading hose, sealants and adhesive compositions, binder in solid rocket propel-... [Pg.1019]

Where pieces of lithium metal are coated with Parylene C, and their subsequent reaction to water vapor follows, the steady-state generation of hydrogen can be controlled exactly by the rate of water transport through the coating (82). Pellets of nitroniiun perchlorate, a potent oxidizer useful as a solid-rocket propellant component, can be rendered less moisture-sensitive and compatible with organic binders by applsdng a coating of Parylene C (83). The absorption of water by... [Pg.9403]

Cationic polymerization of oxetanes has been more recently exploited to prepare a variety of functional polymer materials including functional polymer networks and energetic binders for solid rocket propellants. Polymerization of BCMO has been studied extensively in the past because of the industrial application of this process. After the production of Penton was discontinued the interest in polymers of BCMO ensued from the fact that they may serve as a precursor for various functional polyoxetanes. [Pg.152]

The LP polysulfides are used primarily as sealants and coatings for construction, transportation and chemical protection applications, and as a binder for solid rocket propellants. These uses will not be covered in this book, but there is a use for the LP series as reactive plasticizers for ST polysulfides to control viscosity but not seriously detract from final properties. [Pg.371]

Graham, P. H., and Robinson, C. N., "Analysis of Cumulative Damage in Solid Rocket Propellants by Application of Reaction Rate Methods to the Binder-Filler Separation Process,"... [Pg.392]

During the last decade, the tremendous strides taken in the exploration and exploitation of space have placed new environmental demands on the engineering use of elastomers. In particular, the use of rubber polymers in cryogenic and space applications (in the binder of some solid rocket propellants and in low temperature seals, for example) requires that rubber withstand extremely low temperatures. Under these conditions, rubber can become brittle and cracks can propagate easily through the material. In the case of solid rocket propellants, these cracks can lead to uneven and uncontrolled burning. As one practical technique for increasing... [Pg.409]

The third type of propellent explosive, the composite type, is a more recent development, the purpose of which is to provide rocket propellants of increased thrust, compared with the ordinary varieties. Composite propellants are based on an oxidising solid, commonly a perchlorate, together with an organic binder which both acts as fuel and gives adequate mechanical strength to the mixture. The search for even more energetic compositions continues, but because of the military importance of the... [Pg.169]

The propellant mixture in each solid rocket booster of the Space Shuttle contains ammonium perchlorate ( the oxidizer, 69.6% by weight), aluminum ( the fuel, 16% by weight), an iron oxide catalyst (0.4% by weight), a polymeric binder that... [Pg.35]

A hydrocarbon prepolymer containing terminal carboxyl groups (28) is available to the propellant chemist. These polymers were synthesized to eliminate some of the variables found in the copolymers. The carboxyl groups can be made of the same types with like reactivity. These linear non-branched polymers impart greater extensibility to elastomeric formulations. The chemistry in propellants is similar to the random functionality polymer. As 20 years of the chemistry of crosslinked propellant binders is reviewed, one familiar with the art cannot fail to predict solid propellant formulations using these polymers tailored to the specific requirements of the solid rocket design with the confidence that any discipline of science can be practiced. [Pg.89]

The rockets with solid composite propellants consisting of ammonium perchlorate (oxidizer), pulverized aluminum powder, special additives and binder-cum-fuel such as poly(butadiene-acrylic acid-acrylonitrile (PBAN), carboxy-terminated... [Pg.53]

Solid ammo propellants are difficult to recycle as the smokeless base(s) (NC and/or NG) used in the ammo will deteriorate with age (Ref 27). Solid rocket proplnts in many instances can be recovered, as shown in Table 2. However, the polymeric binder used in solid rocket proplnts is a cross-linked mat which is insol in solvents,... [Pg.173]

It takes a lot of force to get a space shuttle out of the grip of Earth s gravity. Two solid rocket boosters filled with a solid mixture of ammonium perchlorate and aluminum metal, called the propellant, produce most of that force. The rockets also contain a catalyst made of iron oxide, which speeds up the burning of the propellant. Another material called the binder holds everything together. All together, the propellant, the catalyst, and the binder make up the solid material inside the rocket boosters. [Pg.78]

In recent years, the great majority of solid rockets have utilized composite propellants. Most composite propellants are based on a solid oxidizer and a curable liquid polymeric binder. The binder also serves as fuel. Optionally, metallic fuels such as aluminum or boron may also be used.45 The propellant components are mixed together, and then the binder is cured to give the tough, flexible, elastomeric (rubbery thermoset) solid propellant required for modem missile use. An excellent source of information on the formulation of solid propellants is a report by Oberth.46... [Pg.1773]

Composite propellants are solid rocket fuels, consisting of oxygendo-nating inorganic salts and a binder made of plastic. [Pg.112]


See other pages where Binders solid rocket propellants is mentioned: [Pg.9]    [Pg.512]    [Pg.131]    [Pg.240]    [Pg.443]    [Pg.128]    [Pg.64]    [Pg.251]    [Pg.320]    [Pg.512]    [Pg.190]    [Pg.253]    [Pg.129]    [Pg.1003]    [Pg.575]    [Pg.4899]    [Pg.20]    [Pg.309]    [Pg.165]    [Pg.340]    [Pg.345]    [Pg.243]    [Pg.102]    [Pg.102]   


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