archive/ES_0.7769936280510455---------------------------

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: 2023-04-20T09:09:45.882
Launch V∞: [7.352687997708827, -8.681922117152217, -2.1207602984321197] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [2.495782699405155e-6, 1.5772132425734653e-6, -1.1777862312401668e-6] km/s
	V∞_out: [1.7930788406766236e-6, -2.1695487738214965e-6, 1.479501673393297e-6] km/s
	time of flight: 8.314454419739859e7 seconds
	arrival date: 2025-12-07T16:52:09.882
	thrust profile: [0.9435610902150074 -0.6889790910152848 -0.37525509503834525; 0.6125330314098766 -0.14519850365942266 -0.3025875662400548; 0.41775187352335424 -0.014069541470865607 -0.25295759852466093; 0.35816589839772406 0.028675861695275726 -0.2559970619915146; 0.22486497535616878 0.032148685848929756 -0.17487263942911024; 0.012781092922760095 0.0034065488515263795 -0.01422032188463438; 0.02752824170987159 0.010595220087149314 0.023231904565109093; 0.023328569159875346 0.004514737990622438 -0.025342743189141467; 0.007269682918862535 -0.013730536196514473 -0.013114011799484595; 0.0011957178524870937 0.004693717969918204 -0.057263664655228516; -0.0010727231488889578 0.010164281463626502 -0.015931699338663605; 0.003038011795648412 0.038256794494292055 -0.01717818516250667; 0.01562989098080534 0.014002495768139063 -0.08104673324455909; -0.0006409428696990023 -0.042183643135862293 -0.03048003887749874; -0.025437135641617155 -0.02026935535259479 -0.011764448430114857; 0.07038453278160982 0.05820563064395558 -0.006536016690719979; 0.03415749842456408 -0.004769339755575053 -0.043935215938116945; 0.008548774610244309 0.001537681314902996 -0.006949289409662844; -0.0008266677124867164 0.030023470042592967 -0.005636554633070404; 0.03740353786697699 0.010311586937843443 -0.03119176686470388] %

Mass Used: 125.20263540665383 kg
Launch C3: 133.93541668335416 km²/s²
||V∞_in||: 3.1786338734900097e-6 km/s