archive/ES_0.5587350625304599---------------------------

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: 2024-05-12T01:57:41.110
Launch V∞: [8.00235731470902, -5.705343986870514, 0.10054220622999013] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.9884502770460224e-7, -6.474098893816488e-7, -1.8897885624170874e-6] km/s
	V∞_out: [-1.847440833869188e-6, -2.2564956352585673e-7, 7.846697599998949e-7] km/s
	time of flight: 1.834341558544522e8 seconds
	arrival date: 2030-03-05T03:53:36.110
	thrust profile: [0.32144656687020107 -0.005686395454508751 -0.09768926654240323; 0.05981989307051661 0.03409034538755253 -0.06630192920684855; 0.06380400586530999 0.059211616725391755 -0.12433520315678165; 0.04937200231655414 0.06118881629534971 -0.14155311866377207; 0.02006630083413281 0.03217227544864284 -0.08312841311423073; 0.0190213523452368 0.034827390307998286 -0.09732796081582383; 0.014840551460754404 0.03437937196850779 -0.09817653488720686; 0.006889317591317258 0.017077518011741174 -0.056118174981050865; 0.002702165569387325 0.009334276932272257 -0.03357704807493624; 0.002814455387901626 0.009317642561045779 -0.034933983593578466; -3.9384469221349005e-5 0.00047224053263129244 -0.002437986212380226; -0.0023095755983701754 0.00015209433222707243 -0.0036799200895273557; -0.0011116834993707076 -0.0016855016361806967 -0.002829444352647104; -0.002964406725089305 -0.0008949397052070788 0.002461449076096603; -0.002062083707587533 0.0005188436076797558 0.002178648922654564; 9.640256825893196e-5 4.9601694270806726e-5 -0.00040269878714780717; -0.0015257940569766287 -0.0030891491767603 -0.002472201510480593; 0.002455245357668077 2.6599224678949267e-5 -0.0039660150910170635; 0.00017576440922466524 0.0007934219372700898 0.003965205638597732; -0.0011232695391028458 -0.0005878594584839152 -0.0015192817308430076] %

Mass Used: 88.364681825361 kg
Launch C3: 96.59878133603009 km²/s²
||V∞_in||: 2.007480939026432e-6 km/s