Files
thesis/archive/ES_0.5579268478630314
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5579268478630314---------------------------
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: 2024-05-12T01:32:27.036
Launch V∞: [8.002175242599137, -5.594410129659658, 0.1680115328599683] km/s
Phase 1:
Planet: Saturn
V∞_in: [3.064960379220849e-6, -2.6132000814969138e-5, 4.939156866362503e-6] km/s
V∞_out: [-3.788132433054868e-6, 1.438364625491229e-5, 2.3008342626420705e-5] km/s
time of flight: 1.8592169278773242e8 seconds
arrival date: 2030-04-02T22:27:19.036
thrust profile: [0.4286002029867508 -0.0013620582316501084 -0.13075098720036424; 0.06278560473408341 0.036661821657415286 -0.07011199386726612; 0.07171365032521586 0.06866815584955463 -0.14172342923696946; 0.042864254660735124 0.054565753029815096 -0.12780583168282048; 0.031214641215208082 0.04914985033391067 -0.12721200874353217; 0.018051318136591353 0.03385270370519706 -0.09619456025762929; 0.008110176065188488 0.017916701267746696 -0.055522291205751924; 0.004450495378444074 0.01164654158314932 -0.03701202901079538; 0.0029177759297442287 0.006675577789681686 -0.02534253429185726; 0.0008203470778132987 0.002427746925811581 -0.009052828280941812; -0.000562279586896313 0.0011255136005968627 -0.003909640442745755; -7.213892049297413e-5 -0.001398564159691344 -0.0055967686719311325; -0.000600154088295776 -0.0001554279388191596 -0.0010382814561101963; 0.0003058384446208483 0.0023451957031973766 -0.00024077113560838376; -0.0001435625360110728 -0.001412591417388261 0.0015805514169284181; -0.0005569181095084969 0.00034204323397000655 -0.0019885120389492653; 0.0031447908013721533 -0.0009252807692230382 0.002109171540248623; -0.0006613696265909729 -0.0005967062402295642 0.0020359067401852496; 0.0033546005307672454 0.0026280117763101563 0.004775550146659996; -0.0006206275751138688 -0.0017175212560561624 0.002931106903722061] %
Mass Used: 94.64529891440861 kg
Launch C3: 95.36046118727909 km²/s²
||V∞_in||: 2.6770706364798765e-5 km/s