23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5876109836621777---------------------------
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Spacecraft: mySat
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dry_mass: 200.0 kg
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specific impulse: 3200.0 kg/s
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max_thrust: 0.00025 kN
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num_thrusters: 1
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duty_cycle: 1.0
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Launch Mass: 3500.0 kg
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Launch Date: 2023-04-29T11:20:40.350
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Launch V∞: [6.490047970410877, -7.363726176752687, 0.20370412907279356] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [1.1204230343560037e-7, 3.384300248423264e-8, -3.7627177419548915e-8] km/s
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V∞_out: [1.1851611207342117e-7, -3.1660115418599534e-8, 1.4468143864657162e-8] km/s
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time of flight: 1.844382067367015e8 seconds
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arrival date: 2029-03-03T04:10:46.350
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thrust profile: [0.3219880458907638 -0.08445183640904218 -0.11352502647072078; 0.05674226102310718 0.018133658217102885 -0.06749360848743301; 0.0907918009364825 0.05094255575402814 -0.16747046762847492; 0.07128313498914195 0.05361624297608657 -0.1848761694793651; 0.04624033465613945 0.04348107402295378 -0.1582476129421223; 0.024005699646025468 0.02807390334459613 -0.10484384522789157; 0.010125046752561305 0.01574010001742128 -0.05597001107577407; 0.012151806539231555 0.02098401580939068 -0.0777048828241573; 0.009271642126509065 0.007643426424658796 -0.038751563222599796; 0.006314384395733605 0.007954012536408279 -0.03862355030320349; -0.0037800087816584746 -0.002087832171965509 0.016452156095331967; 0.007554183805401041 -0.004247050628187845 0.012166149156028608; -0.004683449855739402 -0.011092015576674545 -0.006203805444796965; -0.005424075559329889 -0.010142207923884554 0.01648723848154191; 0.0247155768087311 -0.042569457444300705 0.021525595685764044; 0.022719822975129852 -0.020717782839158164 0.045085785728060074; -0.004547366610558983 0.0030836547269037103 0.046021433338166225; 0.008783101604753565 -0.0015411778450925297 0.00156871680222699; -0.08483041881919946 0.013104696047582017 0.0505362748456507; 0.0003662263729561129 0.0014954536014915513 -0.0026672409957398677] %
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Mass Used: 123.29050705887494 kg
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Launch C3: 96.3866812366284 km²/s²
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||V∞_in||: 1.2294157578648948e-7 km/s
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