Hey all,
I am Suraj. I am an Aerospace engineering graduate from the
University of Toronto. I am currently working on a constellation design for
Mars.
I am using GMAT to design the trajectory to Mars. I am doing
this by first executing a series of burns to raise the apogee of the Earth
Parking Orbit. But, unfortunately I am unable to design the transfer
trajectory to Mars.
I would request anyone if they could kindly help me with this.
Regards,
Suraj
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