archive/ES_0.5566410051309979---------------------------

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: 2024-05-14T08:54:42.676
Launch V∞: [7.938889175808598, -5.721289888445549, 0.022394513678795636] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-7.126399601975315e-10, -1.0433104624834696e-9, 1.1888897396324165e-9] km/s
	V∞_out: [4.708665918614242e-10, -1.5871095203584354e-9, 2.523624790658423e-10] km/s
	time of flight: 1.8749577785991123e8 seconds
	arrival date: 2030-04-23T11:04:19.676
	thrust profile: [0.383255191431606 0.006364051421795901 -0.11434873060160713; 0.07912463966619467 0.04845184670090699 -0.0874636045875017; 0.059984359105638686 0.05947049867982226 -0.11917254469203618; 0.0312778536995542 0.041558097953147265 -0.09637082603274663; 0.019313731224357273 0.03249360000717824 -0.08518182341095097; 0.01550413260002561 0.03222965544980895 -0.08833115206101098; 0.012882996777312332 0.02933589022891076 -0.0893566660211954; 0.004032017462523549 0.010392579373723256 -0.03494303428819367; 0.0028209133770775436 0.00857952412250399 -0.029821922081028646; 0.0048288801257716125 0.01879364760570276 -0.06576677957090481; 0.00035088792497949017 0.0013884772173374021 -0.0054738182161113355; -9.802475811122548e-5 -0.0002198469876090715 -0.00016047119763963835; 4.095263611168657e-5 0.00024139813787700938 -0.0006865154087776684; -3.238169443340664e-5 0.0005984869055250656 -0.0004305075875650202; -9.589970261021581e-5 0.00023405388670229093 -0.0006315431296312886; -0.0003479669007502964 0.0005700827804409462 -0.0005213707418780502; -5.460411242763069e-5 -5.724666813058794e-5 0.0004728878171271616; 0.0001573301417603173 -0.0003809535382806675 -0.0007432804318140629; 1.1879169077862502e-5 -0.00029569931735530817 -0.0002791215432035887; 0.000255395136063786 -0.0021755543562233283 0.0017859358887216215] %

Mass Used: 90.81671770824596 kg
Launch C3: 95.75962084764312 km²/s²
||V∞_in||: 1.7348807587269639e-9 km/s