Nozzle comprises the most significant component while designing high speed aircrafts. The method of characteristics is
used for designing of supersonic nozzle. A MatLAB program is generated so as to arrive at the parameters of nozzle with respect
to the input conditions. The nozzle was analyzed to find out the properties such as velocity, pressure, temperature and density of
air flowing through it. The aim of the paper is designing of supersonic nozzle that would provide the required thrust that is
needed at supersonic conditions for the aircraft to travel through and to predict the thrust values.
