archive/ES_0.6006528530435701---------------------------

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: 2024-05-07T20:18:00.094
Launch V∞: [6.939694652422336, -7.361312438060483, -1.3203380120927288] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.003284228299013627, -0.005014103851371504, -0.0019306209260854857] km/s
	V∞_out: [-0.0035602249175383702, 0.004589579431587916, -0.0024315473794149444] km/s
	time of flight: 1.233343939738607e8 seconds
	arrival date: 2028-04-04T07:51:13.094
	thrust profile: [0.35031367611278696 -0.14631111235092792 -0.18308609329050585; 0.15850473459879816 0.011993372487135256 -0.19417364331619746; 0.0916478613029878 0.019325757930905338 -0.174626923959689; 0.05397050247008275 0.01748918994916867 -0.13978173313646647; 0.048775755148691965 0.019402932298709156 -0.15519613205689836; 0.07928432465104325 0.04120704875798435 -0.2897823619201835; 0.05979304102111059 0.028453157970958015 -0.24537222200969017; 0.016357608555208954 0.008782928529005326 -0.0738445937579221; 0.011770761919555896 0.005815300494530442 -0.06106724507490666; 0.0029747983858490552 0.0018424846096734197 -0.017019153183855416; 0.0002907015570565931 9.629081156092111e-5 -0.0018331977184753642; 0.00010771271090868189 0.00018675633806387146 -0.0003286507364693072; 0.0001348394118105771 3.997910005289657e-5 -0.0003803959118089231; 6.661768951911194e-5 -0.00010858418229334683 -0.00038896823365406014; 6.840435541158622e-5 -0.000118369577776095 -0.0002680464559449468; -0.00045549539249408643 0.0001268931173395016 0.0002687781143148004; -0.00047914078318691904 0.000237214585565389 -0.00011160136861189466; -6.792136505597406e-5 0.00017763735167810677 -0.00027442713555400736; 3.218725566480254e-5 0.00027603487586948396 -0.0005872940395317294; 0.00043001887294035244 -0.0005796712617445296 -0.0007133557381163448] %

Mass Used: 93.56080686711448 kg
Launch C3: 104.09157514578011 km²/s²
||V∞_in||: 0.00629719700443139 km/s