6a746864_Jet_engine___Engineering__Type
[Description] Intake air is chilled to very low temperatures at inlet [Advantages] Very high thrust/weight ratios are possible (~14) together with good fuel efficiency over a wide range of airspeeds, mach 0-5+ [Disadvantages] Exists only at the lab protoyping stage. Examples include RB545, SABRE, ATREX [Type] 
Precooled jets / LACE
Jet engine - Engineering
Type