30 lines
3.4 KiB
Plaintext
30 lines
3.4 KiB
Plaintext
archive/EMS_1.7964973464843803---------------------------
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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: 2024-12-28T06:03:36.902
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Launch V∞: [1.9113115422257663, 1.0939752985973668, -0.2878460457456588] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-2.396005235896576, 1.5910968460984156, 2.4553745598827215] km/s
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V∞_out: [-0.738879248789918, -1.3198053438616348, 3.466044691382917] km/s
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time of flight: 1.3682159997877434e8 seconds
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arrival date: 2029-04-29T20:03:35.902
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thrust profile: [0.935248482226924 0.9999431292980571 -0.1290404928548267; -0.9999476163597248 0.9999515515170286 -0.24823663597926307; -0.8795731397232727 0.11883370193334312 -0.6198238490789577; -0.47255877270571917 0.8460911087046892 0.5425122446091334; -0.8842186442310318 0.9999442668703385 0.632114794955067; -0.9467809827443692 0.7397804470130911 -0.5827972578364147; -0.9202889335527289 0.8035048754026284 -0.5573817193425457; -0.7074755326919293 0.9999898297887988 0.5385761857415082; -0.778563476191167 0.9440695192200221 0.5088248662337462; -0.999935848670154 0.9999298047351639 -0.5166619290742501; -0.7958311273920875 0.4445916834284018 -0.20253835385960575; 0.799628199463289 0.787390476804687 0.10921619103766879; 0.6775585821251879 0.9999859279862128 -0.056976618126330265; -0.9999708212123471 -0.6329649627446755 0.30597984975011394; -0.3379623142939624 -0.9999302294951131 0.5845511928965047; 0.9999796032643747 -0.12435864928204078 0.05360464346939001; 0.9999735389912225 0.9999936940242244 -0.6858853667949919; -0.9999932115686956 0.9999647789195363 -0.4065818129789695; -0.9999828349783968 -0.9999811809194908 0.2562488369803276; 0.8477193677430503 -0.9999888051388031 0.44654176461357903] %
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Phase 2:
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Planet: Saturn
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V∞_in: [1.687679365659058, -0.3106760396582122, 0.25789343385832764] km/s
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V∞_out: [-0.13000691471236564, 0.7123751472156044, -1.4816590595134704] km/s
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time of flight: 1.3038840000839666e8 seconds
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arrival date: 2033-06-16T23:03:35.902
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thrust profile: [0.9999943154178064 -0.9999793447580555 0.06826775331348747; 0.9999973057987236 -0.7577830174110806 0.09936609510988814; 0.9999978386167154 0.999996910634015 0.12385129639736782; 0.9999970143501956 0.9999984909994136 0.18181347514052054; 0.9999901589869835 0.9999988995839434 0.2578219962691517; 0.676991268524474 0.9999990090764392 0.2880018307347756; 0.20873881951717477 0.9999990450745354 0.2788781951149253; -0.003991942078742135 0.9999990863624453 0.27800285072408; -0.10377137001550704 0.99999919042469 0.26254279367539807; -0.11890106720112337 0.7958208463902771 0.19525684108652674; -0.05544439551611033 0.27388175650220187 0.07106727942943497; -0.036288195450646675 0.14031424139484425 0.03530510666426885; -0.004277653916611693 0.016826893422196152 0.004178638953119427; 9.200391005419325e-5 0.004147286559672669 -0.00015203464796320339; -0.0001527325932206235 0.0003004840617325797 0.00013127411825929072; -0.000154649294574425 0.0010525030105100078 0.0008862518960764552; -0.0009285177821710427 -0.0009909987221447562 0.002296370239222059; 0.0005316057188195457 0.0015595065628119108 0.00010356134502627535; 0.0034358308362445874 -0.0028793310522562256 -6.702429154429191e-5; -0.00030910308067229515 -0.0011037999999218894 -7.645215422836016e-5] %
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Mass Used: 2067.1392010817217 kg
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Launch C3: 4.932749111438047 km²/s²
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||V∞_in||: 1.7353069659620202 km/s
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