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Tonio
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I have to design a space mission to Saturn as part of a course on spacecraft and system engineering. I found a suitable trajectory but, as the Δv is quite high, I would like to adapt it to Ion propulsion.

What are the proper assumptions I have maketo do to make it realistic"realistic" for low thrust propulsion? How can impulse thrust trajectory be adapted to a low thrust system?

The simplest would probably be to find a trajectory with multiple gravity assists, like Cassini did (EVVEJS), but since this is just an assignment project, I haven't the tools nor the time to compute such a trajectory.

  Example trajectory to Saturn employing DSM and Earth flyby

 Example trajectory to Saturn employing Deep Space Maneuver and Earth flyby. Made using NASA's Trajectory Browser

I have to design a space mission to Saturn as part of a course on spacecraft and system engineering. I found a suitable trajectory but, as the Δv is quite high, I would like to adapt it to Ion propulsion.

What are the proper assumptions I have make do make it realistic for low thrust propulsion? How can impulse thrust trajectory be adapted to a low thrust system?

The simplest would probably be to find a trajectory with multiple gravity assists, like Cassini did (EVVEJS), but since this is just an assignment project, I haven't the tools nor the time to compute such a trajectory.

  Example trajectory to Saturn employing DSM and Earth flyby

 Example trajectory to Saturn employing Deep Space Maneuver and Earth flyby. Made using NASA's Trajectory Browser

I have to design a space mission to Saturn as part of a course on spacecraft and system engineering. I found a suitable trajectory but, as the Δv is quite high, I would like to adapt it to Ion propulsion.

What are the proper assumptions I have to do to make it "realistic" for low thrust propulsion? How can impulse thrust trajectory be adapted to a low thrust system?

The simplest would probably be to find a trajectory with multiple gravity assists, like Cassini did (EVVEJS), but since this is just an assignment project, I haven't the tools nor the time to compute such a trajectory.

  Example trajectory to Saturn employing DSM and Earth flyby

 Example trajectory to Saturn employing Deep Space Maneuver and Earth flyby. Made using NASA's Trajectory Browser

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Tonio
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I have to design a space mission to Saturn as part of a course on spacecraft and system engineering. I found a suitable trajectory but, as the Δv is quite high, I would like to adapt it to Ion propulsion.

What are the proper assumptions I have make do make it realistic for low thrust propulsion? How can impulse thrust trajectory be adapted to a low thrust system?

The simplest would probably be to find a trajectory with multiple gravity assists, like Cassini did (EVVEJS), but since this is just an assignment project, I haven't the tools nor the time to compute such a trajectory.

  Example trajectory to Saturn employing DSM and Earth flybyExample trajectory to Saturn employing DSM and Earth flyby

 Example trajectory to SaturnExample trajectory to Saturn employing Deep Space Maneuver and Earth flyby. Made using NASA's Trajectory Browser

I have to design a space mission to Saturn as part of a course on spacecraft and system engineering. I found a suitable trajectory but, as the Δv is quite high, I would like to adapt it to Ion propulsion.

What are the proper assumptions I have make do make it realistic for low thrust propulsion? How can impulse thrust trajectory be adapted to a low thrust system?

The simplest would probably be to find a trajectory with multiple gravity assists, like Cassini did (EVVEJS), but since this is just an assignment project, I haven't the tools nor the time to compute such a trajectory.

  Example trajectory to Saturn employing DSM and Earth flyby

 Example trajectory to Saturn employing Deep Space Maneuver and Earth flyby. Made using NASA's Trajectory Browser

I have to design a space mission to Saturn as part of a course on spacecraft and system engineering. I found a suitable trajectory but, as the Δv is quite high, I would like to adapt it to Ion propulsion.

What are the proper assumptions I have make do make it realistic for low thrust propulsion? How can impulse thrust trajectory be adapted to a low thrust system?

The simplest would probably be to find a trajectory with multiple gravity assists, like Cassini did (EVVEJS), but since this is just an assignment project, I haven't the tools nor the time to compute such a trajectory.

  Example trajectory to Saturn employing DSM and Earth flyby

 Example trajectory to Saturn employing Deep Space Maneuver and Earth flyby. Made using NASA's Trajectory Browser

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TildalWave
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I have to design a space mission to Saturn as part of a course on spacecraft and system engineering. I found a suitable trajectory but, as the Δv is quite high, I would like to adapt it to Ion propulsion.

What are the proper assumptions I have make do make it realistic for low thrust propulsion? How can impulse thrust trajectory be adapted to a low thrust system?

The simplest would probably be to find a trajectory with multiple gravity assists, like Cassini did (EVVEJS), but since this is just an assignment project, I haven't the tools nor the time to compute such a trajectory.

  enter image description hereExample trajectory to Saturn employing DSM and Earth flyby

 Example trajectory to SaturnExample trajectory to Saturn employing Deep Space Maneuver and Earth flyby. Made using NASA's Trajectory Browser

I have to design a space mission to Saturn as part of a course on spacecraft and system engineering. I found a suitable trajectory but, as the Δv is quite high, I would like to adapt it to Ion propulsion.

What are the proper assumptions I have make do make it realistic for low thrust propulsion? How can impulse thrust trajectory be adapted to a low thrust system?

The simplest would probably be to find a trajectory with multiple gravity assists, like Cassini did (EVVEJS), but since this is just an assignment project, I haven't the tools nor the time to compute such a trajectory.

  enter image description here

 Example trajectory to Saturn employing Deep Space Maneuver and Earth flyby. Made using NASA's Trajectory Browser

I have to design a space mission to Saturn as part of a course on spacecraft and system engineering. I found a suitable trajectory but, as the Δv is quite high, I would like to adapt it to Ion propulsion.

What are the proper assumptions I have make do make it realistic for low thrust propulsion? How can impulse thrust trajectory be adapted to a low thrust system?

The simplest would probably be to find a trajectory with multiple gravity assists, like Cassini did (EVVEJS), but since this is just an assignment project, I haven't the tools nor the time to compute such a trajectory.

  Example trajectory to Saturn employing DSM and Earth flyby

 Example trajectory to Saturn employing Deep Space Maneuver and Earth flyby. Made using NASA's Trajectory Browser

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TildalWave
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Tonio
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