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Heat shield

Heat-resistant fib( Heat-resistant polymers Heat-set inks Heatshield Heat shields Heat stability Heat stabilizers... [Pg.466]

A mixture of PhenoHc MicrobaUoons and resin binder has a putty-like consistency. It can be molded to shape, troweUed onto surfaces, or pressed into a core. Curing gives a high strength, low density (0.144 g/cm ) foam free of voids and dense areas, and without a brittle skin. Syntactic foams are used in widely diverse appHcations, including boat flotation aids stmctural parts in aircraft, submarines, and missiles stmctural cores for waU panels and ablative heat shields for reentry vehicles and rocket test engines. [Pg.308]

RCF is sold in a variety of forms, such as loose fiber, blanket, boards, modules, cloth, cements, putties, paper, coatings, felt, vacuum-formed shapes, rope, braid, tape, and textiles. The products are principally used for industrial appHcations as insulation in furnaces, heaters, kiln linings, furnace doors, metal launders, tank car insulation, and other uses up to 1400°C. RCF-consuming industries include ferrous and nonferrous metals, petrochemical, ceramic, glass, chemical, fertiH2er, transportation, constmction, and power generation/incineration. Some newer uses include commercial fire protection and appHcations in aerospace, eg, heat shields and automotive, eg, catalytic converters, metal reinforcement, heat shields, brake pads, and airbags. [Pg.56]

Typical equipment made from tantalum includes heat exchangers, reaction vessels liners, thermowells, and heating elements or heat shields for high temperature vacuum sintering furnaces. Tantalum fabricated parts are found in the manufacturing of pharmaceuticals, explosives, insecticides, dyes, acidic baskets for silver cyanide barrel platers, and in hydrochloric and hydrobromic acid condensers. [Pg.330]

During startup, the baseplate heat shields ate lowered, thereby allowing pump-down through a large gap. The heat shields can then be raised to produce a narrow gap when maximum temperature is requited. [Pg.377]

No fewer than 14 pure metals have densities se4.5 Mg (see Table 10.1). Of these, titanium, aluminium and magnesium are in common use as structural materials. Beryllium is difficult to work and is toxic, but it is used in moderate quantities for heat shields and structural members in rockets. Lithium is used as an alloying element in aluminium to lower its density and save weight on airframes. Yttrium has an excellent set of properties and, although scarce, may eventually find applications in the nuclear-powered aircraft project. But the majority are unsuitable for structural use because they are chemically reactive or have low melting points." ... [Pg.100]

The applications of the unsaturated polyester resins were increased in the late 1960s by the introduction of water-extended polyesters. In these materials water is dispersed into the resin in very tiny droplets (ca 2-5 p.m diameter). Up to 90% of the system can consist of water but more commonly about equal parts of resin and water are used. The water component has two basic virtues in this system it is very cheap and because of its high specific heat it is a good heat sink for moderating cure exotherms and also giving good heat shielding properties of interest in ablation studies. [Pg.708]

Electronic conductivity Flexible conductor of electricity heating elements (resistance heating), shielding of electromagnetic radiation field flattening (high-voltage cables), materials with antistatic capability... [Pg.888]

Plant/process emissions Anti-corrosion coatings heat shields, extractors... [Pg.57]

As a light, strong metal, beryllium holds considerable promise as a useful engineering material, but because of an inherent directional brittleness, a really significant commercial use, e.g. in the aircraft industry, has not proved possible. It has been used to a limited extent in aerospace applications, and it was employed as heat shields for the Project Mercury space capsule. It has also found use in precision guidance systems when fairly pure environmental conditions can be assured. [Pg.831]

The interaction occurs in the reactor (4), which is equipped with exterior heaters and insulation. The coarsest parts of the solids are collected in the collector (5). The gaseous mixture is moved through the connecting tube to the filter (6), which is also equipped with a heater and heat shielding. The solid oxide powder is collected on the filter while the rest of the gaseous components are removed to the heat exchanger... [Pg.312]

Chemical vapor infiltration of carbon-carbon structures (reentry heat shields, rocket nozzles, and other aerospace components). [Pg.193]

Another major computational effort is in the area of metals and their chemistry, which comprises the subject of this manuscript. The studies are directed towards both catalysis and the development of improved materials, such as stronger matrix composites. The materials and gas phase work have some overlap. For example, surface recombination affects the heating on the AOTV heat shield and on the walls of the scramjet. In addition, desorption of these molecules from the walls of the scramjet could impact the chemistry in the flow. [Pg.17]

Fig. 8.38 (Left) The Mossbauer spectrum of the rock called Heat Shield rock, clearly shows with high intensity the mineral Kamacite, an Fe-Ni alloy with about 6-7% Ni (Right) The iron-nickel meteorite Meridiani Planum (originally called Heat Shield Rock ) at Opportunity landing site, close to the crater Endurance. The meteorite is about 30 cm across (Courtesy NASA, JPL, Cornell University)... Fig. 8.38 (Left) The Mossbauer spectrum of the rock called Heat Shield rock, clearly shows with high intensity the mineral Kamacite, an Fe-Ni alloy with about 6-7% Ni (Right) The iron-nickel meteorite Meridiani Planum (originally called Heat Shield Rock ) at Opportunity landing site, close to the crater Endurance. The meteorite is about 30 cm across (Courtesy NASA, JPL, Cornell University)...
For reentry heat shields, ablator materials are well proven. These materials typically consist of reinforced plastics with a density of 0.5 - 1.0 g/cm3. The high heat loads are consumed by the carbonization or sublimation of the ablator. The carbonized material cannot withstand very high aerodynamical loads. When the aerodynamic forces exceed a specific threshold value, the initial slight erosion on the carbonized layer intensifies until the whole layer splits of. This results in an exponential rise in ablation velocity for the unprotected ablator. [Pg.309]

The SP-ablator allows higher aerodynamic loads with lower surface/mass ratio for heat shields, and should be ideally suited for moon, mars, or other interplanetary return missions. These shields are also suitable for cost-effective flight models of winged reentry capsules. A large application potential can be seen for nozzles and combustion chambers or housings of rocket engines. Dornier plans to manufacture a heat shield for the Mirka capsule one meter in diameter. The C/SiC-cover will be fabricated in one piece. [Pg.309]

Literally removal , but applied particularly in space technology to the process of using up the frictional heat developed on re-entry of the vehicle into the Earth s atmosphere by degradation of the heat shield. Certain thermoplastics, thermosetting resins and polytetrafluoroethylene have been evaluated as ablative materials. [Pg.11]

Enclosed ground flares are most commonly used as a supplement to an elevated) flare on the same relief system. The primary reason for an enclosed ground flare is to reduce the visual impact of flared gas combustion on a nearby community. They are often used when it is desirable that all or part of a flare load be disposed of in a way that causes the minimum of disturbance to the immediate locality. They offer many advantages in comparison to elevated flares there is no smoke, no visible flame, no odor, no objectionable noise, and no thermal radiation (heat shield) problems. Enclosed ground flares are typically used for normal process flow (continuous) flaring, but with recent technical advances they are now also used for emergency flaring (AIChE-CCPS, 1998). [Pg.84]

Where monitors are placed close to hazards, such as at helicopter landing sites, supplement monitor heat should be considered for operator protection. The heat shield should not obstruct the visor of the operator and clear heat resistant plexi-glasses have been used at some installations. [Pg.260]


See other pages where Heat shield is mentioned: [Pg.66]    [Pg.66]    [Pg.385]    [Pg.127]    [Pg.192]    [Pg.55]    [Pg.15]    [Pg.285]    [Pg.377]    [Pg.377]    [Pg.336]    [Pg.336]    [Pg.336]    [Pg.949]    [Pg.1190]    [Pg.7]    [Pg.313]    [Pg.206]    [Pg.207]    [Pg.244]    [Pg.102]    [Pg.121]    [Pg.2]    [Pg.16]    [Pg.456]    [Pg.456]    [Pg.771]    [Pg.449]    [Pg.309]    [Pg.84]    [Pg.212]    [Pg.423]   
See also in sourсe #XX -- [ Pg.146 ]

See also in sourсe #XX -- [ Pg.186 ]




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Heat Shielding

Heating and cooling of the thermal shield

Moisture/heat shielding

Radiation heat transfer shields

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