23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5894548171832104---------------------------
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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: 2024-05-08T12:23:52.953
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Launch V∞: [7.194651891685596, -6.81260209585645, -0.5796273304401126] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-0.006544664323325019, 0.0033992664903978544, 0.0002313834156297204] km/s
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V∞_out: [-0.00539521380754203, -0.003010976497136895, 0.004033376646559652] km/s
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time of flight: 1.483292859287872e8 seconds
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arrival date: 2029-01-19T06:58:37.953
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thrust profile: [0.266633502725883 -0.0773926965485505 -0.12023176668292347; 0.1352327929958962 0.02357701864990149 -0.16344443562205113; 0.08507389343480079 0.03149759533845064 -0.16975302866390238; 0.06069993945689674 0.029687462124953934 -0.16958178973684587; 0.04187714761732323 0.024003343426494173 -0.15624029917127324; 0.031738237238559515 0.02146214495729778 -0.15044667646775767; 0.022725036625689178 0.01630969867419624 -0.10199547504065884; 0.00872589863720472 0.0068632699867542364 -0.03511059210426845; 0.03930333438154605 0.03208405936100281 -0.2068236423576905; 0.00029278823758720207 0.00023885147701877072 0.005698449673470026; 0.005527705304415199 0.0034000227916140325 -0.04735863227203936; -0.006319633641407704 -0.002856677748891902 0.0014112433564950513; 0.0003001028033059088 0.005850786270476296 -0.015348141186493155; 0.002409041098956072 -0.004028461801076663 -0.010813896472772153; 0.007863782639211253 0.0029515720166886986 -0.007049167344589819; 0.04092235049381231 -0.020105262272511908 0.01809568783436828; -0.021437888724122705 0.011147762203950506 0.008336123126411686; -0.00466678649955791 0.010223203906949098 -0.013826100212171906; 0.00942336314584752 0.002749445867265338 0.07361756085649288; -0.07026924041234288 -0.002741193329893629 -0.042722424233878384] %
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Mass Used: 113.05252254010247 kg
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Launch C3: 98.51053100119594 km²/s²
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||V∞_in||: 0.007378426801342788 km/s
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