archive/ES_0.5632059488747134---------------------------

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: 2024-05-09T05:16:45.187
Launch V∞: [8.093650411325152, -5.361249343199949, 0.26145978268792236] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [0.0018045495322919277, -0.0009939335968760683, -7.219500711037565e-5] km/s
	V∞_out: [0.001424150793069293, 0.0008954922029882007, -0.0011929427843803515] km/s
	time of flight: 1.874957778741413e8 seconds
	arrival date: 2030-04-18T07:26:22.187
	thrust profile: [0.5398357849174693 0.006910646741517628 -0.1429164604040862; 0.1451815689971349 0.09666887879839994 -0.1428094058421563; 0.05694285153262537 0.06289976394412948 -0.10779129035130924; 0.032649435310912196 0.04905341400213402 -0.09509931608220515; 0.024438758897384137 0.04705098507048967 -0.0995362555252273; 0.010285898906221386 0.023990169438563212 -0.0560425806332443; 0.008615234275133285 0.024302035572642704 -0.06192234191170866; 0.00792391059516295 0.027706120701031078 -0.07177557116793766; 0.0030200552007363444 0.014966196648744167 -0.041144854130330366; 0.0005475826843738421 0.003068023584399395 -0.009161839304317002; 0.00017749278194789545 0.000694669278398923 -0.00111362660857567; -0.0007654236168167179 0.0020975887561238142 -0.004166442021286558; 0.0008041840511218831 0.0013499365386923311 0.00019925903020037933; 0.0004263638503491671 -0.0004931160236271478 -0.0009432953460347376; 0.0003258042228350772 -0.0005253230225787711 0.002035839260173775; -0.0001943807159224465 -5.655911211515578e-5 0.0033861575119249593; 0.0011321676140984794 -0.001607693319400457 -0.000912036642055741; -0.0014468945792160894 -0.004058048425168648 -0.0009452911555603235; -0.0001441059609940585 -0.0009818676292299795 -0.00028814688087243747; 0.0017209033792394165 -0.0027068666372608184 0.002633651333915376] %

Mass Used: 106.88216616159707 kg
Launch C3: 94.3185327186689 km²/s²
||V∞_in||: 0.0020614352108532736 km/s