Take Off and Landing Performance of An Aircraft With Constant/Variable Thrust

The paper pertains to take off and landing performance of an aircraft or a rocket-powered vehicle. The velocity acquired and distance traveled by the aircraft on the runway at any instant of time during take- off and during landing are determined considering variation of its weight due to its fuel consumption. Motion of the aircraft during take- off with constant thrust and during landing with reversed thrust are dealt with and finally during landing by applying thrust equal to drag