Abstract
The purpose of this paper is to find the most optimal design for the PASOPATI cruise missile regarding its endurance, maneuverability, and easy manufacture process. Using pre-sizing methods to design and ANSYS Fluent to simulate the cruising condition, it is possible to find the optimal design for this iteration of the PASOPATI cruise missile. The simulations and flight test yielded several data of the design, such as the flight altitude, endurance, and cruising speed for this iteration. The final prototype design of the missile obtain has a specification as follows: 130 km/h average velocity, 13.33 minute endurance, and 280 meter flight altitude.
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