/home/connor/projects/thesis/archive/EMS_2022-03-30T10:29:57.444/mission---------------------------

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: 2024-07-26T01:19:00.624
Launch V∞: [2.801105685523002, 3.0115505056548346, 0.24159778742184224] km/s
Phase 1:
	Planet: Mars
	V∞_in: [3.2638028052648225, 3.7072432967192297, -0.8111829605867894] km/s
	V∞_out: [0.21900149303391275, 4.961281790968419, -0.625939890484093] km/s
	time of flight: 6.496921386032952e7 seconds
	arrival date: 2026-08-17T00:19:13.624
	thrust profile: [0.001107934241447801 0.0018292007266687126 0.00018565119496341824; -0.0002877684209530748 0.009632735812817879 0.0006406714050849094; -0.0035925789673975825 0.0059022726977168045 0.00036911494627972225; -0.004392271410958318 0.0031496393784072986 8.278924606405449e-5; -0.012079407428345906 0.003283958003507755 -9.305089744052092e-5; -0.015663492755514506 -0.0006101977533498358 -0.0005217677979349034; -0.029609509718733208 -0.00971504175523651 -0.001751767160770895; -0.04705355140306407 -0.030874059949991765 -0.00418091862377451; -0.05338204245020876 -0.05960383790514862 -0.0069506112405576205; -0.045383579040589345 -0.09070049371237078 -0.009483908117466569; -0.022155963117973947 -0.12192130955598213 -0.011451460521380474; 0.02034768398636264 -0.15038741398848862 -0.01256625038597567; 0.08762382671508948 -0.164454623190547 -0.011797458764685229; 0.1749075281973807 -0.14059707594205492 -0.0077920703165491505; 0.2590495954572671 -0.05495769313541083 -0.0002350397416306763; 0.31078395875959064 0.1070497396901885 0.009921413122883931; 0.2315256602857458 0.2917786478366671 0.018335503207980205; 0.04114457125744563 0.356078551965574 0.01876988024197249; -0.1305310921973329 0.33131185148905967 0.014580628212375176; -0.24866263293940324 0.24969498219971523 0.0076663519574371244] %
Phase 2:
	Planet: Saturn
	V∞_in: [4.11359354551261e-5, 0.00023511109390414177, -1.3035059541783836e-5] km/s
	V∞_out: [0.00015465192792359236, -0.00012783566006589105, 0.00012992399487795776] km/s
	time of flight: 2.516930366642689e8 seconds
	arrival date: 2034-08-08T03:03:09.624
	thrust profile: [-0.8184541856940203 0.2442659843524041 -0.004053340354121271; -0.18462760879748796 -0.12954689831551117 0.002015300444404607; -0.018683117374796405 -0.08274850099465172 0.0017810688184995694; 0.18605031572212896 -0.5752577339682567 0.015717634590915026; 0.7899231665527375 -0.831721605721017 0.02629677885724141; 1.0 -0.5024609495919333 0.023603267446363804; 1.0 0.08474233676614021 0.01356986253342746; 1.0 0.7682965866734364 0.0017231700304301538; 0.5800765297826053 0.9025145229862893 -0.012043262027874242; 0.049321884279686014 0.20099767542090913 -0.005729615074688785; -7.198819739380535e-5 2.5490099613361683e-5 8.115187738021953e-7; 0.00010715214961850897 -4.902284353362516e-5 -0.00010380205526740633; 4.5291168568480745e-5 -9.817442721019902e-5 -2.0023042282385832e-5; -0.00010436706033869252 2.1041010802616824e-5 0.00010686288557718574; 4.0651291248531234e-5 1.1722252477788995e-6 -3.811349494694384e-5; 4.8716963058570675e-5 -5.597438718549866e-6 3.23342078594203e-5; -7.451796699985422e-5 1.6611665890359082e-5 9.158000189350461e-5; 2.5080935965254957e-5 3.215621104195173e-5 -4.087712404794397e-5; 1.3855663221283863e-5 -2.730536790197425e-5 4.491673208203398e-6; -1.7292860098192588e-5 0.00017955629586277036 1.0628376982277733e-5] %

Mass Used: 838.6230215492219 kg
Launch C3: 16.973999000466307 km²/s²
||V∞_in||: 0.00023903829073984847 km/s