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00000cam#a22000003a#4500 |
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INGC-MON-09720 |
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AR-LpUFI |
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20221019003847.0 |
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060510s1987 |||a fr||||| |0 0|eng d |
020 |
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|a 0930403231
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080 |
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|a 621.43:629.73
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100 |
0 |
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|a Mattingly, Jack D.
|9 283839
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245 |
0 |
0 |
|a Aircraft Engine Desing
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260 |
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|a New York :
|b AIAA,
|c 1987.
|
300 |
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|a p. 217
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440 |
0 |
0 |
|a Te
|9 270008
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599 |
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|a Ubic.:621.43:629.73 AIAA PRES
|
650 |
1 |
4 |
|a SISTEMA DE PROPULSION
|9 283840
|
650 |
1 |
4 |
|a DISEÑO SISTEMA DE PROPULSION
|9 283841
|
650 |
1 |
4 |
|a TERMODINAMICA
|9 262699
|
650 |
1 |
4 |
|a CICLO TERMODINAMICO
|9 265538
|
650 |
1 |
4 |
|a RESTRICCIONES DEL SISTEMA
|9 283842
|
650 |
1 |
4 |
|a SISTEMA AVION-MOTOR
|9 283843
|
650 |
1 |
4 |
|a ANALISIS DE LAS RESTRICIONES
|9 283844
|
650 |
1 |
4 |
|a ANALISIS DE MISION
|9 283845
|
650 |
1 |
4 |
|a PERFORMANCE
|9 281540
|
650 |
1 |
4 |
|a CONDICIONES DE OPERACION
|9 283846
|
650 |
1 |
4 |
|a DIMENSIONADO
|9 283847
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700 |
0 |
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|a Heiser, William H.
|9 283848
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700 |
0 |
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|a Daley, Daniel H.
|9 283849
|
942 |
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|c LIB
|6 _
|
959 |
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|a MON
|
960 |
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|a 10397
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970 |
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|a Registro convertido en forma automatizada
|
999 |
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|c 9718
|d 9718
|
040 |
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|a AR-LpUFI
|c AR-LpUFI
|