2011.10.02 19:14
RM12 technical engine data
total length - 4.04 m/159 in
max.diameter - 0.884 m/34.8 in
inlet diameter - 0.709 m/27.9 in
engine dry weight - 1055 kg/2325 lbs
bypass ratio - 0.31:1
total compression ratio - 27.5:1
max thrust with afterburner - 80.5 kN/18100 lb
max thrust without afterburner - 54 kN/12150 lb
max.diameter - 0.884 m/34.8 in
inlet diameter - 0.709 m/27.9 in
engine dry weight - 1055 kg/2325 lbs
bypass ratio - 0.31:1
total compression ratio - 27.5:1
max thrust with afterburner - 80.5 kN/18100 lb
max thrust without afterburner - 54 kN/12150 lb
разделы: Авиация
