/home/connor/projects/thesis/archive/EM_2022-03-29T21:29:32.797/mission---------------------------

Spacecraft: mySat
	dry_mass: 200.0 kg
	specific impulse: 3200.0 kg/s
	max_thrust: 0.00025 kN
	num_thrusters: 1
	duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2024-05-23T04:29:27.925
Launch V∞: [3.3948803973755504, -2.4577679470301823, -0.9108626328289409] km/s
Phase 1:
	Planet: Mars
	V∞_in: [-9.533352172826976e-10, -9.477177141496064e-10, -1.6329568148050564e-9] km/s
	V∞_out: [-4.993330429282141e-10, -4.2879092581858787e-10, -2.3614363530159443e-10] km/s
	time of flight: 1.7632014328727353e8 seconds
	arrival date: 2029-12-23T22:18:30.925
	thrust profile: [0.03456534559612611 0.003378817240313221 -0.005847373254693159; 0.00947257573188261 0.018201878458255185 0.007200303057438418; -0.004323909654354275 0.01249526284025378 0.0148773281730713; -0.01158118824683763 0.0035968703342061353 0.015269664673521784; -0.014059676447250516 -0.008412132946442719 0.008604541649422459; -0.005532635332091579 -0.0222637656012968 -0.0034383221186402285; 0.021986188048601012 -0.02106400050803527 -0.008639248086466517; 0.017681089333976076 0.009993783002874504 0.003021725433334957; 0.0019228014351383971 0.011070063719295309 0.013061259255238647; -0.006139542196052064 0.004677076522798168 0.015910259868307026; -0.008545089251963688 -0.004479324701411431 0.011537788412234507; -0.0016877898391656034 -0.011682836725100527 0.0011701415189322448; -0.0003566125916268421 -0.01179761558953741 -0.008519419526240076; 0.014749885872094748 -0.0029190252507672954 -0.0019352156873499635; 0.00424054036493813 0.005291076160963761 0.010144665911928733; -0.002562774524319081 0.0018319412240714573 0.0157273231044577; -0.004535441668234806 -0.00482430642022855 0.014079386327258895; 0.0021824954095405903 -0.011442073033427643 0.0056673371449387985; 0.00910349572655102 -0.00026356393299342343 -0.0060482701344148565; 0.0010618127127533534 0.0009141380026824337 -0.006122360667166782] %

Mass Used: 24.97711287513448 kg
Launch C3: 18.395506929817802 km²/s²
||V∞_in||: 2.1150803439214027e-9 km/s