archive/ES_0.5582385111553505---------------------------

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: 2024-05-13T02:31:47.742
Launch V∞: [7.8774024807270395, -5.862059090178596, 0.2101816533239587] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [4.859785848053225e-7, -6.913207974800158e-7, -6.341171505523664e-8] km/s
	V∞_out: [5.7813127849231905e-8, -2.954215485234778e-7, -7.964007268843853e-7] km/s
	time of flight: 1.837812875656949e8 seconds
	arrival date: 2030-03-10T04:53:14.742
	thrust profile: [0.28623589389640736 0.0020107146992136993 -0.0809524923083333; 0.07078088635367778 0.04558811110295893 -0.07178987487536981; 0.08706826172860835 0.09035489241856363 -0.14969832916228604; 0.037886130599133136 0.053359839633922296 -0.10280604645156818; 0.030893217699051016 0.055842043033024265 -0.1162676232525865; 0.02482884186909009 0.049625058296319316 -0.11146244897026278; 0.014207156047150508 0.03510125034817359 -0.08291545770902795; 0.006674683803683484 0.019219381331320565 -0.05126061741383854; 0.0027987252546384524 0.008057374847148297 -0.021947481832586425; 0.0013272384880022986 0.004695534820583365 -0.015592127022296929; 7.88876695870112e-5 0.002247632398662093 -0.006600780128036748; 0.0014849192022890357 0.0009929926986500552 -0.006767883849638644; 0.0021641610716486752 0.00036756049163183183 -0.0006120847076755524; 0.0009910453768559727 -0.0005856061078448782 -0.0059427556748777866; 0.0023402179213793273 -0.0024993319073937674 -0.0011063909968968074; -0.0020031229952140166 0.0006317813225078724 0.0016357745536532617; -0.0008726747400979774 0.0027123523868270924 -0.003042601786771353; 0.0006112345121948343 2.2978630379946087e-5 -5.718962027173634e-5; -0.004430895482272372 0.0004208440724489476 -0.0005464935681248507; -0.000346138621197969 -0.0018998064315019947 -0.0035697729345717717] %

Mass Used: 88.5868624874688 kg
Launch C3: 96.46138294750402 km²/s²
||V∞_in||: 8.474200112836819e-7 km/s