23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5722260918659717---------------------------
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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: 2023-04-29T20:53:49.783
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Launch V∞: [6.483742208735468, -7.376382357154615, 0.026633501853375607] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [5.065887763291213e-7, 0.000169120559523567, -0.00010246369206712065] km/s
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V∞_out: [-9.421581735675477e-5, -0.0001697173562827695, 3.411995329293851e-5] km/s
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time of flight: 1.8476879838133124e8 seconds
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arrival date: 2029-03-07T09:33:47.783
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thrust profile: [0.3317757882867481 -0.08742278607389777 -0.11266512459967307; 0.05396952729416926 0.015353722192758303 -0.05823319370415226; 0.06725055317818836 0.03686028195017193 -0.11835540284736024; 0.04380560449503716 0.0327723927681535 -0.10916640285463189; 0.05509164929272785 0.04985784721890868 -0.17077147558055858; 0.030842844063408474 0.03250057538457453 -0.1199928099094051; 0.007129938581510352 0.011040284332360472 -0.04612298765062194; 0.004418709279614309 0.00710927757568007 -0.03445154247819217; 0.01778395402922857 0.024515496399804704 -0.10570243676036294; 0.008119468259820165 0.009205005023882976 -0.04228870876206575; 0.0009455067433678495 0.0011049578806048045 -0.0065262988831272; -0.00485499764232693 -0.002708757946068235 -0.0037930046586778384; 0.01847557721673204 0.001573793714157608 0.007853259716063028; 0.0005027977275157662 0.001728157021416917 -0.007263507970825747; -0.002202247834841863 -0.0003554501229188175 0.0027323392658324007; 0.006163724839356371 0.0104075911347386 -0.00665952729554513; -0.012128735872144797 -0.02423547512028097 0.008476289476932818; -0.01146823849484239 -0.010453389206265398 -0.003568584773260006; -0.002355864224989661 -0.00523220427678208 -0.0177286886615009; -0.0013555372009282484 0.02135180662304421 -0.04357343106011266] %
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Mass Used: 104.9683793753793 kg
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Launch C3: 96.45063905170075 km²/s²
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||V∞_in||: 0.0001977392942178625 km/s
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