44 lines
6.4 KiB
Plaintext
44 lines
6.4 KiB
Plaintext
/home/connor/projects/thesis/archive/EMMJS_2021-12-03T11:37:09.379/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: 3500.0 kg
|
|
Launch Date: 2023-02-26T04:10:12.359
|
|
Launch V∞: [-4.841701064906604, 3.475969740428134, -4.8994214190507] km/s
|
|
Phase 1:
|
|
Planet: Mars
|
|
V∞_in: [0.02729198924983877, 5.017291114045934, -2.960466892478738] km/s
|
|
V∞_out: [-0.7796648643413417, 5.029374064409783, -2.8347788324016983] km/s
|
|
time of flight: 1.9570320002726743e8 seconds
|
|
arrival date: 2029-05-10T06:10:12.359
|
|
thrust profile: [0.51200489277245 0.1491712750305638 -0.5617898782756465; 0.5985472817937932 0.4314745458970473 -0.29088252333102027; -0.45166509877363964 0.5194585980906682 0.5146294788199312; 0.390520290781806 -0.5192326236428068 0.4429840782407487; 0.5160025656800347 0.43684584169735574 -0.4960808446595455; 0.5098504634472127 0.5199893315046626 0.4441400784392527; -0.49987113488322754 -0.47893620910952606 0.48036085120848565; 0.5368410355569405 0.5166822047764457 -0.4858670271400151; 0.44238316289905827 0.547824927494726 -0.4656337244770621; 0.21668892035180595 0.6021857778661118 -0.19651661385197258; 0.4341377302277037 -0.16678624993961083 0.5761938702855823; 0.5718885908183827 0.5536579188076003 0.33795675555520704; -0.39527664332753926 0.5814857962643089 -0.4679595952307845; -0.008428218148373924 0.5415048084721836 -0.45110046854424596; 0.33161932673220734 -0.45295582817342434 0.46836263037592774; 0.5280374896116378 0.5764518977818923 0.3342129870989262; 0.3107502688966615 0.5511548090736831 -0.5014473758638118; 0.07343276836897304 0.6646323168301356 -0.33765386861899715; -0.5980335383406491 -0.5746723266973839 0.15575901290142588; 0.590900565213738 0.39693261331727714 0.20472515338144043] %
|
|
Phase 2:
|
|
Planet: Mars
|
|
V∞_in: [3.0241033936172084, 1.6385004369573686, -5.605711794771172] km/s
|
|
V∞_out: [2.4283811769402535, -1.1475844477691648, -6.003401620464895] km/s
|
|
time of flight: 1.1737080029703692e8 seconds
|
|
arrival date: 2033-01-27T17:10:12.359
|
|
thrust profile: [-0.1768137656168143 0.3393511738335891 -0.353565456723947; -0.15954083659688176 -0.5487799730055659 -0.24022806443793981; 0.5157742145013325 -0.7252600963065111 -0.4938126290082077; 0.698500596084941 0.03900690309877106 -0.23316637699244064; 0.6365913895344839 0.20777317872832707 -0.2830962364627441; 0.5861304271928349 -0.1184358449845895 -0.4564142893293172; 0.6860855423630463 -0.5456724995449903 -0.44617293698271493; 0.6670491113213445 -0.38498567211274926 -0.3230834818585812; 0.5283999818464645 -0.09570871485046831 -0.478027472175741; 0.6580560949600205 0.46722570225829474 -0.11535896533777851; 0.5612619202113102 -0.1931961652510376 -0.4400901944952552; 0.4590177925799 -0.6932770941014383 -0.5144556676853405; 0.7561006651195121 -0.6660301702898956 -0.558073578122206; 0.7758630959701225 -0.08472708630272804 -0.41036611726373284; 0.566096622638857 0.7122289950338151 -0.11214847640185667; -0.4306590268194921 0.4288485227605312 0.2105331105689206; -0.5085374829983493 -0.516980326040015 0.16675646570585556; -0.5812762098132924 -0.6592114464112737 -0.39525785227607435; 0.3559795650447502 -0.8283244516408661 -0.5816275654619777; 0.7220122543976706 -0.8709955103801817 -0.5752271662039113] %
|
|
Phase 3:
|
|
Planet: Jupiter
|
|
V∞_in: [5.060776761478531, -2.65457156740014, 1.2093916749224973] km/s
|
|
V∞_out: [-4.655218918764466, -2.2507227956970843, 2.7173192390054806] km/s
|
|
time of flight: 7.437600000965603e7 seconds
|
|
arrival date: 2035-06-07T13:10:12.359
|
|
thrust profile: [0.5554028628906259 -0.8562653819570508 -0.4353192179666242; 0.6836770270628973 -0.8068634065800825 -0.40691024348661053; 0.6938434264699962 -0.7253280301253697 -0.3838170511550203; 0.645874750163326 -0.6289501430894447 -0.3499668164482744; 0.5889993418389312 -0.5421974665324047 -0.3250231983004846; 0.521131977446493 -0.4767106284566455 -0.3139270110389849; 0.44907608028844187 -0.42835191134595757 -0.30427273241100156; 0.3771619836123307 -0.38593020022499613 -0.29345181442595814; 0.30758537653438345 -0.34138417397604953 -0.2806050625679753; 0.24090511199415704 -0.2908278788914028 -0.2653604699658747; 0.17676587080788508 -0.23266346298480622 -0.24755096472050972; 0.11564885705822119 -0.16792372723278565 -0.22685867498381254; 0.07637432600785862 -0.10221693792171678 -0.20194486428807676; 0.019753903444897154 -0.058193667702053815 -0.18756658332981802; -0.044040327145306354 -0.00021057373845115093 -0.15565868544825787; -0.1020149066984689 0.047297427488451 -0.11989375229021738; -0.15572852811033114 0.08561531859322227 -0.08266441800646043; -0.20039007901031922 0.11872106917143616 -0.04576729741807346; -0.24124782668690306 0.1511930898415435 -0.009960538806793113; -0.28349017928188214 0.1924753920006318 0.02615368339855036] %
|
|
Phase 4:
|
|
Planet: Saturn
|
|
V∞_in: [-7.256385977948657, 0.7771719462797614, -0.785892915072424] km/s
|
|
V∞_out: [-5.9473393974944736e-6, -7.362203906933263e-7, 6.306068555232033e-7] km/s
|
|
time of flight: 1.4662439997163886e8 seconds
|
|
arrival date: 2040-01-29T14:10:11.359
|
|
thrust profile: [-0.18959418256753224 0.13412715420236315 -0.043410183532822624; -0.19766571870169566 0.1372601657158578 -0.037968113030145044; -0.1971783405485536 0.129832118307628 -0.04157452597322259; -0.19192072677853972 0.11752160892327206 -0.04544882251204915; -0.18096355607909057 0.10099613325234727 -0.04845756455495175; -0.16440940142977603 0.0827695902679096 -0.0501168011338542; -0.14159683191947461 0.06939209018313232 -0.04938123378650775; -0.11494734465063888 0.05950353242028259 -0.04787565574075916; -0.08842871021960914 0.05331851047785903 -0.04243441932918664; -0.06244946835797671 0.049895056937498274 -0.03534701683264976; -0.0380028875571515 0.047256901837732644 -0.02725064975669285; -0.01886788294008128 0.04286456425792469 -0.019192970894846496; 0.0054749884299889135 0.041277048472854974 -0.010750429199969911; 0.02389959629376803 0.03888123568193434 -0.0015386535754099552; 0.0428231915186611 0.03753775483224003 0.00740487148339779; 0.06481451674589596 0.03713565978563092 0.014580239918154077; 0.09005525246175461 0.0369062161152353 0.018428292697994248; 0.1201760127678751 0.03212421201511818 0.04118543343400019; 0.15404590862831494 0.02789044310966664 0.043771491647338116; 0.18466591121075765 0.02447914444489793 0.052012952789042624] %
|
|
|
|
Mass Used: 2528.0301016677718 kg
|
|
Launch C3: 59.52876507974255 km²/s²
|
|
||V∞_in||: 7.3400791119043935 km/s
|