archive/ES_0.6964135801004295---------------------------

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: 2023-04-27T08:24:35.331
Launch V∞: [6.189010312123412, -9.032184657165224, -2.257040997448067] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [-0.09962360408532854, 0.06675142282625997, 0.1235609090274915] km/s
	V∞_out: [-0.055657988734206076, 0.1167842569417847, -0.11360493482400895] km/s
	time of flight: 8.888783968570797e7 seconds
	arrival date: 2026-02-19T03:28:34.331
	thrust profile: [1.0 -0.912555178180571 -0.5345321390902776; 0.44267124304884364 -0.13351974999836913 -0.3154157791361182; 0.07799931141046376 -0.006375428530351986 -0.08393734979378419; 0.03843163734563034 0.001313775911391553 -0.053241223845234616; 0.03136554698216834 0.003046908617080231 -0.05350999950151559; 0.017412369497967643 0.0021744805330009245 -0.0309058202451753; 0.004239686727695683 -0.0002734365101370622 -0.006591461156908401; 0.007227702851295962 0.0022872629495891946 -0.011344530632068845; 0.001151757240453521 0.0010946437582688789 -0.009229859005840144; -0.0013819076476665193 0.0017457243857838243 -0.0033097707197890097; -0.0006672138492093108 -0.0006780179900488716 -0.0011870796035920882; -6.59808512147083e-5 -0.001324996641033391 0.0009615291788712434; 0.000534536203146787 -0.002932370176073119 0.004219036773188727; 0.0014177532266098952 -2.8316464269005854e-5 -0.00030038637606611806; 0.003403085587491225 -0.0007867301180634335 0.0017989417489220048; 0.00020218592624084505 -0.0033792814434725578 -4.590392085585678e-5; 0.0017400506569416347 -0.0017977226108663045 0.0007085495433876183; 0.0008371218467089906 0.0002017951864594764 -0.0014373855890759462; 0.000547342586592261 0.00013926234365551683 -0.0011214664117306285; 0.0061909035437434515 -0.002660745251404345 0.00014557728237261371] %

Mass Used: 83.44159618213826 kg
Launch C3: 124.97844238886219 km²/s²
||V∞_in||: 0.17218569388883753 km/s