I recently acquired the Megatraveller CD ROM. On page 32 of the COACC, it lists the TL 10 Fusion Rocket engine for a fixed wing aircraft burning only 5 liters per hour of fuel to generate 195 Tons of thrust. For comparison, the same page states that the TL 8 High Bypass Turbofan engine for a fixed wing aircraft burns 3840 liters per hour of fuel to generate 50 Tons of thrust. I found nothing on this in the errata. Does anyone know the correct data for the Fusion Rocket engine? It sounds too good to be true.