30 lines
5.9 KiB
Plaintext
30 lines
5.9 KiB
Plaintext
archive/EMS_2021-10-18T18:22:44.188/mission---------------------------
|
|
|
|
Spacecraft: mySat
|
|
dry_mass: 200.0 kg
|
|
specific impulse: 3200.0 kg/s
|
|
max_thrust: 0.00025 kN
|
|
num_thrusters: 1
|
|
duty_cycle: 1.0
|
|
Launch Mass: 2500.0 kg
|
|
Launch Date: 2023-06-03T18:39:41.030
|
|
Launch V∞: [1.4528171939898546, -0.7402553543714421, 0.7198063620664785] km/s
|
|
Phase 1:
|
|
Planet: Mars
|
|
V∞_in: [-0.09755558196699422, -5.3760255002748165, 1.7853084087216329] km/s
|
|
V∞_out: [2.8879492524068695, -4.6008182394117, 1.6098548998016842] km/s
|
|
time of flight: 1.362669505585263e8 seconds
|
|
arrival date: 2027-09-27T22:35:31.030
|
|
thrust profile: [0.014609011290562383 0.023526054638363506 0.06586887507050274; -0.06429218902505592 0.0003875221488966037 0.025068287312389175; -0.07722181604763545 -0.0164935736357545 0.006484354491785095; -0.05418670199657678 -0.022646287453370457 -0.08113490766539934; -0.0506166491243181 -0.04748837806503002 -0.10084803864225915; -0.06035477738922144 -0.05527195771007038 -0.11674201815059983; -0.08962934751172418 -0.07120699904034963 -0.11701738451143721; -0.11623494873904305 -0.12424723770859708 -0.10180855594746802; -0.10825232081959534 -0.20934236634778766 -0.061949505438447156; -0.04450437764051239 -0.29053535177066586 -0.0052401903439667245; 0.10858287109159012 -0.33531112320191925 0.050573299933059424; 0.2917560473211387 -0.28130087234888473 0.09141235049602812; 0.363552744102322 -0.0653888495734924 0.1119765464717816; 0.30023433762797985 0.1586653839712532 0.09775032797542846; 0.13381909610838597 0.25349442292502145 0.050962207120256495; -0.05561879073077972 0.25047891650044996 -0.010222224987169614; -0.18500289408520745 0.1838459648234384 -0.06501054068816181; -0.2633626984585559 0.06740350331400906 -0.10552803707472241; -0.3015544455362966 -0.08340867428702191 -0.12617391907275552; -0.2980095390699629 -0.2392946380342424 -0.12629505951265152; -0.23148023546107505 -0.3749701410683523 -0.10783217167181713; -0.07894071469307276 -0.4623486266693046 -0.07144480401887415; 0.16028862146595801 -0.4876815213223878 -0.02061179953627845; 0.3842493049278076 -0.42962504947168956 0.03643143668725137; 0.4974283466407711 -0.25309214932909857 0.08670208210950218; 0.5081883636716127 0.056291903479390164 0.11796471433830415; 0.4250685878142111 0.3104706473083573 0.11729541002445289; 0.23197825493691604 0.41240232472252586 0.08768881929972193; -0.0341851598132791 0.4223722506927382 0.03849582457917256; -0.24433348749555175 0.3610375051148529 -0.012354553480072056; -0.3655218556786849 0.24731588669440885 -0.05623949962000103; -0.4321022352880162 0.08131757252852433 -0.09105682922783279; -0.4452688895396858 -0.1283039646949706 -0.10285727576535383; -0.44828910931376825 -0.33298162270769677 -0.09536559717749803; -0.38974387016899464 -0.4806378526366322 -0.0761592904485703; -0.2542461950012492 -0.5780829896901187 -0.049525518351972206; -0.002525096494219299 -0.6161727076821379 -0.01995455750679716; 0.301010770990131 -0.6164209241411417 0.009878755441330631; 0.5087877254811393 -0.5664346000510313 0.037058328078365066; 0.6087744242184348 -0.43501726760054543 0.05873876234455045] %
|
|
Phase 2:
|
|
Planet: Saturn
|
|
V∞_in: [3.5677789156110467, 2.7323128411776048, -0.5598992896398332] km/s
|
|
V∞_out: [1.0115880934192722, -1.8761487227720552, -2.6595170315286336] km/s
|
|
time of flight: 1.920830007442836e8 seconds
|
|
arrival date: 2033-10-29T02:58:51.030
|
|
thrust profile: [0.7881817473912547 -0.3389570569515258 -0.0694603003835884; 0.7545518240816476 0.16890824057359943 -0.05140667750465577; 0.6716820532694702 0.45119947667699334 -0.040831401900494044; 0.5658986867834962 0.5296028081006117 -0.034430918767449886; 0.4601436552292838 0.5475873435366672 -0.029817337051142707; 0.37050165220345244 0.5161676453402835 -0.025404500044545482; 0.29817541281347015 0.48289541289681487 -0.02110019963638442; 0.24169921197011807 0.44481524027189223 -0.01678514557739015; 0.19799125176255297 0.40636791170350123 -0.012722544258577625; 0.16428420463735924 0.36992082529127546 -0.008920457561270273; 0.13698227078716912 0.3355724366720239 -0.0053512238222314734; 0.11629130909242422 0.3060842336647084 -0.002489926881812709; 0.0987526125187477 0.27798808469115466 0.0002579142494755621; 0.08496841699409616 0.25449290869954533 0.002544966213217921; 0.07231123011723056 0.23076223747312233 0.004936145151231231; 0.062055600081047414 0.21341224350289537 0.006970017100223167; 0.052971371729138676 0.19639984729795226 0.008912261502883554; 0.04491958739793588 0.18126531579006996 0.010694634190802039; 0.037516267473304735 0.16812010997359988 0.012304447489889469; 0.031205986014880224 0.1567127760397761 0.013579987889275308; 0.024964383575319944 0.14503758963145616 0.014795695571499715; 0.019486740557152424 0.1362257015826171 0.015574564807330962; 0.014158411905557245 0.12789681805235922 0.016125715357447532; 0.00908308339622475 0.12028286897448305 0.016371544848018692; 0.0044102283095267085 0.11345559090550508 0.016294319554773354; 0.0005966776869157249 0.10751884153271778 0.01572311388373797; -0.003970105448958323 0.102279781501889 0.014937124392557143; -0.007640861057492033 0.0975984328130423 0.013618238849724724; -0.01144277898857823 0.09288700411779988 0.01215176103351869; -0.014785099224280838 0.08873083508061831 0.010231512465192402; -0.017730681821126432 0.08523320581633666 0.007925597342036909; -0.02102250152959055 0.08175375259513366 0.005511476561201909; -0.024837202491318048 0.0784357240142721 0.002989652933139063; -0.02916815773485098 0.07561185185811473 0.0004038081994905193; -0.03510340581821502 0.07180740263170013 -0.0021818331399174945; -0.039579141117804674 0.06726211579068186 -0.005175977417815043; -0.04013452158968421 0.06358356010989077 -0.009080952414709772; -0.03743321426527317 0.05894746602403381 -0.0148014675802013; -0.03482398229591096 0.04786083701811494 -0.02059203468208998; -0.034121069580906806 0.04002789158453891 -0.017780319292331873] %
|
|
|
|
Mass Used: 844.8639343830812 kg
|
|
Launch C3: 3.176776987699523 km²/s²
|
|
||V∞_in||: 4.528583339995187 km/s
|