Klimov RD-33

RD-33
Klimov RD-33 turbofan engine.JPG
RD-33 expuesto en el Museo de la Fuerza Aérea de la Bundeswehr.
Tipo Turbofán
Fabricante Bandera de Rusia Klimov
Primer encendido 1974
Principales aplicaciones Mikoyan MiG-29
Mikoyan MiG-35
HESA Shafaq
JF-17 Thunder
Coste unitario 2,6 millones de $[1]

El RD-33 es un motor aeronáutico turbofán desarrollado en la OKB-117 liderada por S. P. Izotov (ahora OAO Klimov), su producción comenzó en 1981. Es un motor de reacción turbofán con postcombustión de la clase de 8.000 a 9.000 kgf (78 a 88 kN) de empuje.

Contenido

Variantes

  • RD-33
  • RD-33B/NB
  • RD-93
  • SMR-95
  • RD-33 Serie 3
  • RD-33MK

Especificaciones

Características generales

  • Tipo: Turbofán
  • Longitud: 4,2 m
  • Diámetro: 1 m
  • Peso en seco: 1.055 kg

Componentes

  • Compresor de baja (LPC): 4 etapas
  • Compresor de alta (HPC): 9 etapas
  • Turbina de alta (HPT): 2 etapas
  • Turbina de baja (LPT): 2 etapas

Rendimiento

  • Empuje: 81,3 kN con postquemador / 50 kN sin
  • Consumo específico: 75 g/kns 188 g/kNs con postquemador
  • Relación empuje a peso: aprox 8:1


Véase también

Motores similares

Enlaces externos


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