37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EVMS_2021-12-14T07:13:59.762/mission---------------------------
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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: 2023-02-16T05:05:32.419
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Launch V∞: [3.453247666372975, 3.054378572063566, 0.6410592621774811] km/s
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Phase 1:
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Planet: Venus
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V∞_in: [4.153079961936853, 5.459670821339341, 1.7440959409843952] km/s
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V∞_out: [6.710988704381646, 0.6372991451166926, 2.1574305475746165] km/s
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time of flight: 6.880360130276513e7 seconds
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arrival date: 2025-04-22T13:12:13.419
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thrust profile: [-0.16468330421268426 0.2189329295052185 -0.010873373523340836; -0.37786012024771315 0.20083778181188183 -0.006424325713147286; -0.5363839840515389 -0.21650601709151382 0.008355901825288066; -0.1834968949564447 -0.5561458893436484 0.022693080099818807; 0.25056844492648533 -0.3743357803658322 0.01765926371738561; 0.1740788365495075 -0.23152478296259496 0.027396199892226875; -0.2272240445300924 -0.12216723581853697 0.0019073418117069496; -0.30400700667720765 0.03385256284712383 -0.0074809413195897415; -0.4432437436533131 -0.12491757205634534 0.001436858833454895; -0.25527810292667125 -0.47170642997472956 0.01723278603053477; 0.10898711472363787 -0.35128780086659317 0.02104164145167786; -0.12804417889558464 -0.30272123758944086 0.0327809201214705; -0.18015320445436095 -0.3135806255343057 0.013653240243077786; -0.2094636680250507 -0.23126228233960147 -0.011785210455459378; -0.33027685949511737 -0.16914499178629147 -0.004386004892518824; -0.20190263120461807 -0.36731341845462673 0.011628082895590211; -0.1902112001660596 -0.2648905855353262 0.025952835297502176; -0.31508347575033296 -0.29163705829609193 0.023397543761390662; -0.20963477326342633 -0.39341238177599347 0.016402862738082804; 0.002812966706787112 -0.3622400996934989 -0.0021344748372502283] %
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Phase 2:
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Planet: Mars
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V∞_in: [7.040278950309005, -0.7501648907703503, -1.1912371523753373] km/s
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V∞_out: [6.888311168909946, 1.6990426218863528, -1.100876807493356] km/s
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time of flight: 9.342629092297508e7 seconds
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arrival date: 2028-04-07T20:57:03.419
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thrust profile: [0.356740070161183 0.09173310552676897 0.016574996568492047; 0.19378678269157593 0.4003618878297842 0.0381127321481018; -0.14928159447866768 0.4268446644300027 0.0715397377621758; -0.36113057153024997 0.33270767280174496 0.0696644041484723; -0.40841967844319355 0.20314247070355662 0.06584645395451007; -0.3961511181475026 0.051309814044093315 0.0613267572370165; -0.26862361927193956 0.025846072419724607 -0.008417903267850992; -0.13635376645426722 -0.285269600012018 -0.08480671134086627; 0.48172274225702855 0.03908288821073942 -0.05302198385151616; 0.29736513890266103 0.49380435392567307 0.005932551117785213; -0.1985367964283465 0.530870057786597 0.0443930796666557; -0.42331702745207156 0.43958981624872456 0.059782969970213436; -0.5008191025029283 0.2545821318245874 0.06513111946463424; -0.5090995507101782 -0.08132366596204624 0.05557971290084116; -0.4365235221818152 -0.3526326460862695 0.02944186352246856; -0.2428244049915453 -0.47913502242306927 -0.001429975852898112; 0.2965174674673905 -0.4998400318898462 -0.025394379226107915; 0.5581409602767857 -0.2670720924249945 -0.039037417950486986; 0.5404240598856603 0.4588278322563326 -0.025739054026010875; 0.26481365444928556 0.5889586368264279 0.004310453551953653] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-1.768248852275849, 8.741237951612776, -0.10565185114199886] km/s
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V∞_out: [-0.5689195906105274, -1.1835291484022944e-5, -0.00015076538393807672] km/s
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time of flight: 2.0647184294271883e8 seconds
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arrival date: 2034-10-23T14:14:25.419
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thrust profile: [-0.4118350568502539 0.7397165160046664 0.03650850663151651; -0.5341616982673818 0.5894274810704492 0.048162894586397755; -0.4755846337249282 0.43205141226513055 0.041845478429139625; -0.39146679855903316 0.2793885116422214 0.02666641123567999; -0.29760210470836107 0.10001617063364038 0.005246077036260758; -0.12498798746952003 -0.08547038452801747 -0.03186649737115955; 0.6012927333188255 -0.45651427473844913 -0.006324492609029606; 0.7279077782996053 -0.47845321826514736 -0.032106373666422404; 0.7991128821218656 -0.008283851491542838 -0.07299734954029101; 0.7175587921889662 0.7765717901964799 -0.0800061252435837; 0.3713835047173401 0.773068311463042 -0.038433384532840224; -0.22213951903671245 0.7320154781062939 -6.0672070416028177e-5; -0.3604362859233379 0.6654377220105319 0.014630889316898951; -0.36946080731663716 0.5882623820858978 0.019090223705502275; -0.34750278679765795 0.49839847471976123 0.019927901000876793; -0.31336540870223417 0.3875868492542638 0.019145167045154086; -0.275163205347443 0.2458793980758599 0.017720554190660976; -0.22860840531216062 0.04253129834335439 0.015609619947715278; -0.1634843649420853 -0.13471729070541885 0.012551273723230135; -0.0964949439134174 -0.2770815913878259 0.009813568018480465] %
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Mass Used: 1584.5276313627078 kg
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Launch C3: 21.665104884415 km²/s²
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||V∞_in||: 8.918918501922759 km/s
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