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Objective: Design a propulsion system for Gokturk 3 satellite. Assume the following mission requirements:
• Satellite mass (excluding the propulsion system): 1,200 kg
o Initial orbit: 700 km 28.5 degrees circular
• Orbital Maneuvers:
o Inclination change: -2 degrees
o Orbit raising to 800 km circular orbit
All the other requirements of the project are given in the word.doc.