/home/connor/projects/thesis/archive/EM_2022-03-29T22:38:25.802/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: 2024-10-07T17:37:26.448
Launch V∞: [-1.132800064227913, 4.057296625668816, 1.8160423657393692] km/s
Phase 1:
	Planet: Mars
	V∞_in: [-0.09025126720242063, -0.16294649165165395, 0.002018029101130675] km/s
	V∞_out: [-0.18204756492089805, -0.026081869886201665, -0.0286582298370937] km/s
	time of flight: 1.7138821243684784e7 seconds
	arrival date: 2025-04-24T02:24:27.448
	thrust profile: [-0.001053336200227854 -0.00028654474915887655 -0.0003820424031938627; 0.0008512529608243817 0.0008846317646016004 0.00025282033285603365; 0.00042096876484458586 -0.000407673670480482 -0.000928628092675361; -7.585307650884643e-5 -0.00013518461742213344 0.00156643510514752; 0.0008460627785635593 -0.0007843263217494761 -0.0007202803479853547; 0.002018749793184083 -0.00017983404176264242 -0.0006659097248956292; 0.00040668294946816447 0.0009420606711834561 -0.0007751842339076142; -0.0002948940003770048 1.1828072211327191e-5 -0.00013445879115795128; -0.0004411373325257146 0.002302823369497903 0.0007032460495624283; -0.0004305359949988352 0.0003086368359122586 -0.00012577020060691192; -0.0004796057040344445 0.00048325375373444216 -0.0012858708318398222; 0.0007082846291908338 0.0014131843493881463 0.0012334716036545182; 0.0007516628476279127 0.00019283672154011742 -0.00047698959544296255; 2.8585166048847224e-5 0.0004721397839283915 -0.0004494052618972365; 3.140121868826565e-5 1.8672409758238784e-5 -0.0010892419657405827; -0.0012387600934636242 0.0010224726118372646 0.0005096784526400515; 0.0004830392791164112 -0.00018504611294579005 -0.0007919144470676173; -0.0002823515956750592 0.00015118295801919124 -0.0004211043216927825; 0.000699667738192727 0.0008572250810665738 -0.00044787467026235686; -0.0013106710074165672 1.8187501171149852e-6 -0.0013087579926788614] %

Mass Used: 0.17400800233144764 kg
Launch C3: 21.04290176833857 km²/s²
||V∞_in||: 0.18628183704988058 km/s