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thesis/archive/ES_0.5814989700060318
2022-04-18 10:59:25 -06:00

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archive/ES_0.5814989700060318---------------------------
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: 2023-05-11T18:01:56.379
Launch V∞: [6.222941244329981, -8.097290235740175, -0.37830550874521574] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.000759594549750657, -0.0008324359360318916, -0.0007906378159229647] km/s
V∞_out: [0.0008987147839283911, 0.0004127783490474374, -0.0009587886522597127] km/s
time of flight: 1.8749577783334565e8 seconds
arrival date: 2029-04-19T20:11:33.379
thrust profile: [0.10450129642334803 -0.04101195588411613 -0.0565846532927551; 0.026817683349757537 -0.003006545681199387 -0.04750204809036376; 0.03194730210404488 -0.0039026901973350184 -0.09620134991059028; 0.03215027678335359 -0.006408107919240902 -0.13187971064794962; 0.027022906429893127 -0.007942159082425217 -0.13755085819284535; 0.021557667835074897 -0.008469558212640506 -0.12832186063873932; 0.015815336507602907 -0.007823497673106364 -0.10644850677013969; 0.009104528572024212 -0.005277392463798262 -0.06765957991813695; 0.004533855892999096 -0.0029552473309875696 -0.035623632552891575; 0.002072172078452334 -0.0014587387514032786 -0.016823500390251513; 0.00013757586211982 -4.421067402598201e-5 -0.00037466873806831354; -8.809225899046244e-5 -0.0001316128316758093 -0.0008905207319915944; 0.00039682418245149894 -0.0005102863459595915 -0.0005107223181859803; 0.00015726458926769692 -0.00024494018775572934 -0.0005175202469987778; 0.00029042451531939226 0.00023293710066856583 -0.000424975654588182; 0.0010761874890582673 0.0006083753241496954 -0.0005103407077641287; -0.000297816661669885 2.109367884439765e-5 -0.0009773460844355233; 5.3108445294797394e-5 4.3356416479562544e-5 -8.191435152672406e-5; -0.0004085824671729002 -0.0005606262957715943 -0.0013433747944269002; -0.0018764152668373326 -0.00037630777815904896 -0.0001819493832476128] %
Mass Used: 69.21583696453445 kg
Launch C3: 104.43422195014331 km²/s²
||V∞_in||: 0.0013766051080740733 km/s