30 lines
6.0 KiB
Plaintext
30 lines
6.0 KiB
Plaintext
archive/EMJ_2021-10-17T21:08:51.754/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: 2500.0 kg
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Launch Date: 2024-07-06T16:53:06.420
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Launch V∞: [2.823260136727537, 2.381108515747835, -1.1737954184426584] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [2.902861479885485, -0.1301588187286526, 0.5669523646795902] km/s
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V∞_out: [1.2390632915772526, -2.6409219673539095, 0.5046925355113366] km/s
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time of flight: 8.406297685905933e7 seconds
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arrival date: 2027-03-06T15:42:42.420
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thrust profile: [0.028228817867935244 0.053182566407982926 -0.005054663926030233; 0.005180991851963007 0.0691267924422102 0.013038631124657914; -0.01835805901316754 0.07797668784621446 0.018887537170958094; -0.04313315513357476 0.0809829176156282 0.021806553767181762; -0.06988530553795076 0.07712475685245705 0.02268972139668397; -0.09160758234108493 0.06543179558733468 0.022920454069390864; -0.1098123230541046 0.048341432708635626 0.02151601256114964; -0.12416200616133212 0.027738217207134444 0.020347163167160537; -0.12404293183146138 0.004594899202334194 0.01781507236173057; -0.129155106428887 -0.018581222723093913 0.015298565117590243; -0.12594445263101686 -0.04108652934367247 0.012181435889810483; -0.10860936010879739 -0.05785302549837615 0.00890973312478223; -0.10393797281280423 -0.07897218026647294 0.00494505413203299; -0.08521938934261546 -0.09058792826776481 0.0012801713442578088; -0.06698239018925649 -0.10245050522157627 -0.0027148245589721583; -0.045044579632776124 -0.10478276823574494 -0.006031882980462719; -0.019818627599936134 -0.11139252552545366 -0.010000432210139557; 0.0066242503051877994 -0.10782329745516596 -0.013383858391826825; 0.029766766476497408 -0.09304788741910684 -0.014621131811926025; 0.05750430178483703 -0.08012010231118588 -0.01650664280943883; 0.07827347208136144 -0.05537964439127179 -0.016320867265109163; 0.09261947560772284 -0.02299543299729445 -0.01455858393469228; 0.09914023902019727 0.01591579482167083 -0.011193947076876463; 0.09063940115885241 0.05898855695612724 -0.005929896204151002; 0.06562724891334723 0.09677747829323594 0.0002817010626295331; 0.03846970252523767 0.12968738800889829 0.00626592931214816; -0.014035225318634879 0.1361208554208243 0.01176008272041749; -0.05863663148385729 0.13663351842555724 0.016096346897994468; -0.09798980203153297 0.12317156391252018 0.018711388911181882; -0.1287382519404487 0.10136466288547417 0.020224984128762728; -0.15229270558056937 0.07559496903524954 0.02091790105954753; -0.16565847087960348 0.04430480310028889 0.020006565230859367; -0.17099526669102774 0.011725103749944139 0.017625143996990278; -0.17465152376404056 -0.021415939415702346 0.016435553138393833; -0.1662103957877246 -0.053109462009637225 0.013646899820177756; -0.15857493205251574 -0.0829239406367925 0.01060486274179457; -0.14547673456334026 -0.10870102348055301 0.0070249122604629346; -0.12091234656594241 -0.13188792443501676 0.0032459735017410355; -0.09964673314350471 -0.14990800833225337 -0.0006435420389953807; -0.06918156970036916 -0.16214795228903475 -0.004493281692042949] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [0.9794144953440926, -1.6587037436890903, 0.05654746348233507] km/s
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V∞_out: [-1.442616061274985, 0.20917386745107652, 0.7533137730861299] km/s
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time of flight: 2.4817766374856794e8 seconds
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arrival date: 2035-01-16T01:57:05.420
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thrust profile: [-0.06322475657399902 -0.4936412371250037 -0.005248083444931861; 0.31392545590226156 -0.5120378343745214 -0.012018965544909697; 0.47194614797631196 -0.3385154091925152 -0.013619738208986319; 0.47127775359634877 -0.06255509378665888 -0.01058423533560999; 0.4308172696537082 0.1701852677638707 -0.006203039675066387; 0.32923840143306177 0.29483054460219477 -0.00246666320173045; 0.18955789797808223 0.3399680173098846 0.0003099824286388989; 0.0431089416132578 0.3578274755748262 0.0018852825335888795; -0.09203547110389645 0.33673084856938534 0.0028123031626823957; -0.19872369663279124 0.30432208370956937 0.005854340007928506; -0.2753934814720275 0.2414543286714742 0.0024528411856131562; -0.31670942879503544 0.16271231757680057 0.002127443207860713; -0.3438228796584529 0.07027601644482545 0.0007277441848606637; -0.3353653444000856 -0.039387445962680574 -0.00019633155682904487; -0.3265117073926918 -0.1386710081315292 -0.001357629546225422; -0.2884243829888734 -0.21671499306159014 -0.0018452201988479967; -0.23036032285216418 -0.2676059176999412 -0.001905654329530745; -0.16057203251898639 -0.300550042644732 -0.0011930641633508003; -0.08352138790234072 -0.31051056059986193 0.00042115538205838047; -0.0031878721141613163 -0.29349054473899483 0.003091115280434996; 0.05993893256943912 -0.26032674719704674 0.0053269904930877045; 0.1034231109686185 -0.22911382612325418 0.008553162275029957; 0.12379922022945494 -0.17899312791607294 0.010143198405040877; 0.12784230457331472 -0.14426714773205093 0.0040528976528373915; 0.12695750648192003 -0.10884078117445839 0.011386843321909838; 0.11632236195028951 -0.07978366535429325 0.011224249977602942; 0.1031692845424281 -0.05338815831167443 0.011316629317471546; 0.09543517501110639 -0.03876712479073331 0.011620292225683908; 0.07781476589416222 -0.023192140146226708 0.01123805571020805; 0.07615001373781183 -0.012209894306577049 0.011721969728096762; 0.06551619304657824 -0.0009017074150139166 0.011163886816134776; 0.053829199564220935 0.009053864413266161 0.010089338822184992; 0.04517243555412592 0.018953951227581048 0.008744400898323478; 0.03335908443255013 0.02708335225021901 0.00691716108064741; 0.022240908301819448 0.03578671309503256 0.004813124702550245; 0.009013884979404078 0.04121040835432829 0.0029897347712111487; -0.002318672961402956 0.04893760947231614 0.00045620814999721825; -0.015217962371449503 0.05539099372635576 -0.002059133107886335; -0.028357882479279055 0.059346949102816016 -0.0037261443912981157; -0.04093441818667926 0.0601240161765365 -0.004707490891211125] %
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Mass Used: 587.7637081769217 kg
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Launch C3: 15.018271247758625 km²/s²
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||V∞_in||: 1.927108839335395 km/s
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