Hello folks,
I am having a little bit of a dilemma over here... My dissertation is due in on the 22nd of July, and for the past 2 months, I have been getting very weird results on GMAT. I am working on a hybrid electro-chemical propulsion system in the low-Earth-orbit. Somehow, I get the same results for the chemical rocket, ion thruster, and hybrid propulsion system. I also got the same results when I used 1, 2, and 4 burns... same results when I used constant thrust, same results when I used constant amount of fuel. Something is definitely wrong and I have been trying to tackle and troubleshoot the problem, but, unfortunately, no luck. I reckon GMAT is just ignoring my input values for the thrust and isp.
Anyone got any ideas on what might be happening?
Thanks in advance!
Best regards,
A.
I am having a little bit of a dilemma over here... My dissertation is due in on the 22nd of July, and for the past 2 months, I have been getting very weird results on GMAT. I am working on a hybrid electro-chemical propulsion system in the low-Earth-orbit. Somehow, I get the same results for the chemical rocket, ion thruster, and hybrid propulsion system. I also got the same results when I used 1, 2, and 4 burns... same results when I used constant thrust, same results when I used constant amount of fuel. Something is definitely wrong and I have been trying to tackle and troubleshoot the problem, but, unfortunately, no luck. I reckon GMAT is just ignoring my input values for the thrust and isp.
Anyone got any ideas on what might be happening?
Thanks in advance!
Best regards,
A.