archive/ES_0.5605472272782301---------------------------

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: 2024-05-11T07:35:22.261
Launch V∞: [7.892926426677194, -5.680227447296816, 0.12006163243606052] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-1.6954168992149495e-9, -1.6720733270774625e-9, -1.943894190854001e-9] km/s
	V∞_out: [1.1410256689162797e-11, -3.535262733873365e-11, 6.092222950458916e-12] km/s
	time of flight: 1.859758693100561e8 seconds
	arrival date: 2030-04-02T19:33:11.261
	thrust profile: [0.4343258857613348 0.01289125781793145 -0.10007648991848643; 0.12340184279912034 0.08795208245524054 -0.10797740818028384; 0.047878439902197964 0.059480392338645015 -0.08636379001824729; 0.037522391707089764 0.06357768206139447 -0.09782725040420531; 0.015096539092754793 0.03632562743617328 -0.06190935397280046; 0.027177531319125942 0.0771619834096038 -0.1324194522827905; 0.0074216568823389575 0.02744154659806753 -0.05250783986869373; 0.006525547408933895 0.030726805705565897 -0.061278205944576294; 0.00400311754529153 0.02136872840315104 -0.04667923074456893; 0.0016656793938261817 0.011363055904259222 -0.02796840902223478; 0.0012084862587956487 0.014642812084872317 -0.04129999299550627; 0.0005142276979811721 0.006090568267924427 -0.016352848725427194; -0.00012508289161780432 -0.00036840726162654195 -0.0002036426716727127; 5.010806593898827e-5 2.350226848404338e-5 0.0011283291993822498; -0.0028489288974432136 0.0012750610961193187 0.000149039025779185; 0.0001979861332168749 0.00010472695493748816 0.00048329599670917723; 0.0002529669750614495 -0.0015023976260849698 -0.00032857844813086157; 0.0004460439793345531 -0.0002852498533702395 0.0014947132757420073; -0.0014004877962048874 -0.0006969783590175587 -0.0006625001835830904; -0.00025871449021075714 -0.00018452542941653982 -0.0004381667394975433] %

Mass Used: 102.26859550891368 kg
Launch C3: 94.57768622554653 km²/s²
||V∞_in||: 3.0739213227575395e-9 km/s