archive/ES_0.560525852490877---------------------------

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: 2024-05-18T08:09:42.648
Launch V∞: [7.914347179318701, -6.019872097810366, -0.03999692365348044] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [1.092884330266422e-6, -3.638962837026846e-6, -1.0275666551097795e-5] km/s
	V∞_out: [-9.966552360640912e-6, -1.0248116654586006e-6, 4.4580437320214775e-6] km/s
	time of flight: 1.874957777798284e8 seconds
	arrival date: 2030-04-27T10:19:19.648
	thrust profile: [0.2230507609050875 0.0004292056256291622 -0.07568953440590867; 0.0416233620151584 0.022711983076455635 -0.051216469703687525; 0.04978001118478353 0.04395121330475413 -0.11045737143279427; 0.03223807166592525 0.03687122512896524 -0.10638486898220866; 0.03300739227317162 0.04790590795615277 -0.13976187707662327; 0.011096130326921064 0.01597673974139551 -0.06051968255797275; 0.011675626775582704 0.022011437971001933 -0.08481877927259673; 0.008050329417921939 0.01964334406747146 -0.08109538888950071; 0.0033687012223005135 0.0076246514176061585 -0.03045221084044534; 0.0009445361071728339 0.0030399125053542373 -0.012041997691621027; 0.001930306810481272 0.004654395224346136 -0.024611935594622075; -9.038834874895573e-6 0.00023982780278542876 -0.0006376709664880693; -0.0019282566168357153 -0.0008544872438367508 -0.0006969533291311136; -0.00204638251794161 -0.0009876722326605848 -0.0015300774594088412; 0.0004478780843060866 -7.889597502095617e-6 -0.0006831162105905538; 0.0001787903223300494 -0.0003785984272296096 0.0022044606658822704; -0.004134556796206276 -0.003908075684170739 0.001298992457965057; 0.0005580853024708231 -0.0022467557212176767 0.000542510531275689; 0.001344680652537415 -0.0024508279562628515 -0.00341737020354285; 0.002745266773451587 0.0025862357555927256 0.0024941847510948642] %

Mass Used: 77.16227980701342 kg
Launch C3: 98.8773511026874 km²/s²
||V∞_in||: 1.0955627310106639e-5 km/s