/home/connor/projects/thesis/archive/EM_2022-03-29T22:29:19.608/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: 2024-10-10T01:24:19.159
Launch V∞: [-1.361280774218496, 4.248905515475195, 1.6131303371846983] km/s
Phase 1:
	Planet: Mars
	V∞_in: [-1.3206429765527528, 0.04508054081073763, -0.10860236471971149] km/s
	V∞_out: [1.3258015388055073, 0.008890670618699885, -0.015202352520394155] km/s
	time of flight: 1.6044052824580787e7 seconds
	arrival date: 2025-04-13T18:05:11.159
	thrust profile: [-9.649476733530478e-5 -3.874129604104022e-5 0.0001243676257598534; 0.00017944991783773494 -0.0003021068710903314 -0.00023906829442885233; -1.2520197657221369e-5 7.529839362963302e-5 5.22491643077963e-5; 6.0473365960938625e-5 -0.00010443015036179195 0.00013074051319186437; 0.0006044516898117107 -0.00017952114259198458 7.975422345770218e-5; -1.5105320951034641e-5 5.488422632601538e-5 -3.480125630187902e-5; -0.00035693490512667196 -2.9324170471654634e-5 9.386409045588269e-5; 0.0006536233376695634 -0.000323215551438777 -0.000991075858075292; -0.00048048705998534366 -0.0008846136053753608 7.485312552148982e-5; 0.0002457539906734169 2.3610783147200267e-5 0.00031354855012369744; 0.0003084291416236774 0.00030133549870160124 0.00012216085485925468; -3.145870054396133e-5 9.600064248608948e-5 -0.00017139285888021958; 0.0002323428803906647 -0.0003932431132474737 -0.00038269549666544874; -9.648756923300717e-5 7.371414257236465e-5 -0.00010492608262327025; -0.00016513882219009883 5.681301427250039e-5 -0.00023413816734468073; 0.0001688227002363334 3.9296604381294236e-5 -0.0002465079878323193; 4.223349001330004e-5 0.00018462477409466818 0.0004274596352430292; -7.266996009870076e-6 -0.00023420474628868667 3.054421622059266e-5; 4.4599716714522025e-5 -0.00015080232626015259 -0.00017624139057002226; 2.058233894174994e-5 -2.9681895453803056e-5 0.00010285445493880417] %

Mass Used: 0.04864906937473279 kg
Launch C3: 22.508472910438055 km²/s²
||V∞_in||: 1.3258674897215847 km/s