archive/ES_0.5566019691002949---------------------------

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: 2024-05-16T02:29:49.950
Launch V∞: [8.021699044520817, -5.752221790435776, 0.06331268053948352] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [0.0002724969774579242, 0.0001915574377838364, 0.012530708805207832] km/s
	V∞_out: [-0.011694795249521597, -0.003975707144540381, 0.00213316942489075] km/s
	time of flight: 1.8749577787491933e8 seconds
	arrival date: 2030-04-25T04:39:26.950
	thrust profile: [0.28495651909375325 -0.01110513620576851 -0.1057923105682466; 0.07754327820716317 0.037204936740850326 -0.1014681248616661; 0.03202633356416473 0.023558354710407764 -0.07583949768371191; 0.039077218549460724 0.035868029051525877 -0.1322776091889598; 0.03308456834412289 0.03667129102460999 -0.14804838120989156; 0.01576914995465892 0.018692484605488807 -0.08808072802739021; 0.005237689191798305 0.006645808109634825 -0.035037516578579515; 0.007045163579496689 0.009639579541698761 -0.054962975848279555; 0.00402905071685159 0.005579785635051347 -0.03446419875880498; 0.0021803840096826293 0.0032375208141675813 -0.020303950012354955; 0.0007742263422909088 0.000942399866883276 -0.006413471997769904; -0.0006947182864249202 0.0006525191242631504 -0.0019591264000990995; 0.00020383918620010211 0.0009442447793243495 -0.00020614433584093558; -0.0002450954261624832 -0.000713066052057468 -9.071169538088985e-5; 0.00017115135912938918 -0.00034931664808378256 0.00013612174375342723; 0.0008716179606212026 0.00030601545839085834 -4.0663732936094005e-5; -0.00018984395856919316 -0.00016067107648134912 0.002031217914709764; -0.0014604416944170924 -8.862749599291452e-5 -0.00047864950456458113; 0.0038670380005153587 0.00043516518194716333 -0.002522561016813623; 0.00044385876894278303 0.0019823000769147014 0.002981311135618534] %

Mass Used: 80.97059971765066 kg
Launch C3: 97.43971958274744 km²/s²
||V∞_in||: 0.01253513510160968 km/s