archive/EVMJS_archive
---------------------------
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: 2024-04-20T12:58:59.053
Launch V∞: [-8.920597561322369, -7.117372634919496, -1.472451871563068] km/s
Phase 1:
	Planet: Venus
	V∞_in: [-5.017961509289203, -5.654947873213361, -1.4864114620218827] km/s
	V∞_out: [-7.390394917247088, -2.021337895911062, -0.8148956710919548] km/s
	time of flight: 4.572852817115571e7 seconds
	arrival date: 2025-10-01T19:21:07.053
	thrust profile: [-0.21862938814794752 -0.05580927018043333 -0.036914761844326786; -0.24413346338652692 -0.02556655529310196 -0.03840768064934617; -0.26465223193143633 -0.031988862192285895 -0.03672328500867164; -0.2775111471212138 -0.0533843665242742 -0.03463858507707235; -0.282355262314745 -0.07982445428959191 -0.033636788586472385; -0.28050912409469175 -0.10607204371684377 -0.032167717475040075; -0.2733689146909765 -0.12962521272658228 -0.03161077625553056; -0.26190711303703673 -0.14877589397585794 -0.030649321801181607; -0.24697067176434023 -0.16354203331437878 -0.029534650090164597; -0.22916216500741854 -0.1736646300332696 -0.02774354605279356; -0.20930307239303453 -0.1793556553425328 -0.02624057086532488; -0.1881341647769172 -0.18020842931174086 -0.022018620586908344; -0.16781156346033524 -0.1755305190264814 -0.017713311035217196; -0.1529314715768468 -0.16133304311878607 -0.011294101805393433; -0.1439292332041623 -0.13894686830886066 -0.005512101036767262; -0.13595373894772989 -0.11376326317155387 0.008492968124788823; -0.14161082765712693 -0.0633805633113515 0.026736612907202688; -0.14271356865834361 0.024062134302168376 0.04098391846668108; -0.1414981556176295 0.035473208118311124 0.03720171942581438; -0.13060050476893825 0.04192201790827888 0.030084566679769147] %
Phase 2:
	Planet: Mars
	V∞_in: [-9.28829223014179, -7.607789338281241, -0.2942705558666007] km/s
	V∞_out: [-8.317437974959708, -8.663545949996019, 0.030785372299447233] km/s
	time of flight: 5.8747531161094815e7 seconds
	arrival date: 2027-08-12T18:06:38.053
	thrust profile: [-0.174672404758962 0.02506293138125133 -0.02426121230831768; -0.05008204073446195 -0.07279118574621102 -0.08129060414874276; 0.18941101625787235 -0.07952903306738271 -0.10689582281590368; 0.35705302923506294 0.027307923111368104 -0.0479794442058468; 0.41799317552955584 0.12801887957214292 -0.029898349295167635; 0.4511914489377908 0.23489263829219467 -0.020213669874118333; 0.4656012050626349 0.3325378259130575 -0.014159348767163066; 0.4657014753978555 0.41280917091846614 -0.013135235235423743; 0.45029470699103086 0.4771859548843401 -0.012168900825375072; 0.4106794937152572 0.5294663391131441 -0.011594787023374607; 0.33819071474272516 0.5678785558859125 -0.010353193332547849; 0.2001630795815917 0.5937428427734591 -0.00709996654137991; -0.035108210746352266 0.6005435960325474 -0.0011602329790232843; -0.29361875930485426 0.5723600768872681 0.008300256500510222; -0.4548836328849185 0.4770722319186511 0.014296267759918423; -0.5113471724292226 0.19706675000368873 0.01697398652461365; -0.4134871925757221 -0.2340982056617441 0.01763457992701102; -0.17230637273503518 -0.34708241891449854 0.032309764753320355; 0.1190741484482409 -0.3404978442614275 0.03287368817385319; 0.30168780764812786 -0.2869031294203351 0.028403718812872233] %
Phase 3:
	Planet: Jupiter
	V∞_in: [-2.998311290651761, -5.22937520865022, 0.1407756821047572] km/s
	V∞_out: [-2.856148992180316, 5.306598853387247, -0.19607428788923498] km/s
	time of flight: 1.4159768899978405e8 seconds
	arrival date: 2032-02-06T14:48:06.053
	thrust profile: [0.37857744177475117 -0.5722922563923073 0.022790081593862904; 0.4498819042137626 -0.33368177218590706 -0.006756732610181868; 0.45137346520621063 0.2646268898149342 -0.06715401087102708; 0.3370898120722347 0.5147560334694927 -0.0942931710827749; 0.10406019537076351 0.6331750657513396 -0.10357703864723887; -0.3067722620848112 0.6948315815503575 -0.0862070073278207; -0.5894971893625187 0.7222874275705 -0.047061967331428964; -0.7438646368242161 0.7031736402976893 0.007847733426895626; -0.8153797919927924 0.4618300002958423 0.06963851455772195; -0.8054139924887445 -0.5908908470157955 0.097381115730603; -0.6892129370491469 -0.7264006520777874 0.08776061857832115; -0.45980277149808124 -0.7029156090490672 0.07926634239802542; -0.23430875626887712 -0.6386864247061581 0.07411409321833815; -0.11447347572705899 -0.5560871561049769 0.0680750057792953; -0.06705788386230047 -0.46200938046607043 0.06022766091205061; -0.049086029532628715 -0.35725786450463903 0.05078115410828272; -0.04044489185865085 -0.23996050920253587 0.04039683492314978; -0.034110498545589486 -0.10823424969630317 0.03211353029920855; -0.025504423988764145 0.06607493481717405 0.015337634169998754; -0.016379042728758193 0.201103314416455 -0.001097801876741442] %
Phase 4:
	Planet: Saturn
	V∞_in: [-3.7553623927693303, 3.8045661430805238, -0.0017497584909869502] km/s
	V∞_out: [0.00016771014375336496, 0.02190103395006303, -0.00015322066785738935] km/s
	time of flight: 2.0181733919676498e8 seconds
	arrival date: 2038-06-30T11:10:25.053
	thrust profile: [0.18326801514146682 0.11845670033224177 -0.0016084372043512012; 0.1675872421589649 0.14235871799128041 -0.002787329388980011; 0.14198390921850934 0.16511394888691344 -0.0037731022920933425; 0.10352323696814321 0.18228824596062612 -0.004414585252525113; 0.052724231521741716 0.18616944898352478 -0.004616750142156716; 0.0011654214657718389 0.1688827891674893 -0.004589773974233177; -0.031151502893950005 0.13429086557793365 -0.0048861485136074976; -0.0387542725070042 0.09962903031836343 -0.005697801228946161; -0.032764472688793025 0.0752213826812925 -0.006648655387876376; -0.02303421181483975 0.059664277716287864 -0.007393815905338262; -0.013366915890350172 0.04886766638458846 -0.007849749770643184; -0.004273656127481105 0.04004011769410306 -0.008128123571266301; 0.005274989439679697 0.03136991809704025 -0.008359024971909892; 0.01659789890620425 0.02034976567361285 -0.008341112112060404; 0.027347691011068397 0.0015674507187789124 -0.007372599601001636; 0.03221036017744093 -0.01353396250128953 -0.004949290348108288; 0.03641858295092107 -0.025405796803472054 -0.003362734977936097; 0.04156323966242008 -0.03555478122658915 -0.002142996490186938; 0.04760308383336786 -0.0450888885925399 -0.0011510722358481168; 0.05448090196904719 -0.0542737048917187 -0.0003050212878129177] %

Mass Used: 1175.3239683910674 kg
Launch C3: 132.40216858944106 km²/s²
||V∞_in||: 5.345790240905041 km/s