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060510s1963 |||a fr||||| |0 0|eng d |
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|a AR-LpUFI
|c AR-LpUFI
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|a 629.76
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| 245 |
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|a Materials for Missiles and Spacecraft /
|c John C. McDonald...[et al.]
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| 260 |
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|a New York :
|b McGraw-Hill,
|c 1963.
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| 300 |
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|a xi ; 442 p.
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| 505 |
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|a General criteria for the design and manufacture of missiles and spacecraft - Materials at cryogenic temperatures - Extreme high temperature materials - Materials for thermal protection - Compatibility of materials - Choice of materials and fabrication technoques for pressure vessels - Fracture of pressure vessels -Temperature control of spacecraft - Evaporation effects on materials in space - Lubrication - Nuclear materials and problems - Materials for direct conversion - The economic aspects of materials and their applications in missiles and spacecraft
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| 650 |
|
4 |
|a MATERIALES DE MISILES
|9 286060
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| 650 |
|
4 |
|a MISILES
|9 270214
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| 650 |
|
4 |
|a NAVES ESPACIALES
|9 286061
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| 650 |
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4 |
|a DISEÑO DE MISILES
|9 286062
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| 650 |
|
4 |
|a CILINDROS A PRESION
|9 284279
|
| 650 |
|
4 |
|a LUBRICACION
|9 264839
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| 650 |
|
4 |
|a PROTECCION TERMICA
|9 286063
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| 650 |
|
4 |
|a TEMPERATURAS EXTREMAS
|9 286064
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| 650 |
|
4 |
|a METERIALES NUCLEARES
|9 286065
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| 700 |
0 |
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|a Parker, Earl R.,
|e ed.
|9 286066
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| 942 |
|
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|c LIB
|2 ddc
|6 _
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| 999 |
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|c 10226
|d 10226
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