archive/ES_0.5759811976951041---------------------------

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: 2024-05-04T03:22:08.935
Launch V∞: [7.281305352347205, -5.669656937228578, 0.651146029432309] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-1.8144082665737452e-9, 1.3100870150541078e-9, 3.566557931195864e-10] km/s
	V∞_out: [1.5640951080964024e-9, -1.4327680218399688e-9, -1.2040625893106209e-9] km/s
	time of flight: 1.8571420458577853e8 seconds
	arrival date: 2030-03-23T14:38:52.935
	thrust profile: [0.999999972954426 0.0083887902431605 -0.12278897062580661; 0.44619782683759573 0.3145764409735176 -0.21164280531804439; 0.13340022404531088 0.16392084271774998 -0.13763511739786075; 0.061043807510275064 0.10828991598849314 -0.10263841273621689; 0.0371724922607515 0.0899635850858565 -0.09198063590392302; 0.016415526851795585 0.05231708271291638 -0.058485264729959706; 0.005843883788734285 0.024487019041548732 -0.029733803732709993; 0.003836977272532631 0.020972908280198852 -0.02707047400194581; 0.0015168950152778912 0.012034034955902528 -0.01653071667749158; 0.0005126900221916826 0.0022911883822415444 -0.001882795769230505; 0.0012218787264714768 0.0004637707950976947 -0.0009903307575769948; -2.1419797069248446e-5 0.0007036893677066676 -0.0007595475554741166; -0.0010225916174297176 0.0004555624550349653 -0.0004617246901912884; -0.0020144870569198006 0.00016964684458069062 -0.000983821183405697; -0.0003086092399232806 -0.0007815298584802384 -0.0018691338471416097; 2.8589323854376835e-5 0.0007566077693655276 -0.0008758008260953147; 0.002919983286166899 0.0002571501151864056 -0.0013281835368362473; -2.7357038647113412e-5 0.0007264201174066193 9.379126537454224e-5; 0.0014205535020786937 -0.0018446864365619636 -0.0015614408132531288; 0.0005685871345772497 0.001826591058318955 0.0008360434891899356] %

Mass Used: 172.72401397644853 kg
Launch C3: 85.58640857162966 km²/s²
||V∞_in||: 2.2661881430257034e-9 km/s