30 lines
5.8 KiB
Plaintext
30 lines
5.8 KiB
Plaintext
archive/EMS_2021-10-18T16:59:17.315/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: 2023-04-28T02:09:03.278
|
|
Launch V∞: [-0.28345133710132847, 1.0743854420236858, -0.7978154104086252] km/s
|
|
Phase 1:
|
|
Planet: Mars
|
|
V∞_in: [-3.9967794624862174, -1.796615553688495, 0.18069271269193854] km/s
|
|
V∞_out: [-1.548984364644081, -4.0995103503572965, -0.1751138267279006] km/s
|
|
time of flight: 7.294333712413637e7 seconds
|
|
arrival date: 2025-08-19T08:11:20.278
|
|
thrust profile: [0.27129342959528535 0.3105357481410173 -0.13776198909539616; 0.2857943315505697 0.37422284577893283 -0.07741685575269751; 0.29147675327956785 0.43700523965167776 -0.03795847200581804; 0.26195889887210855 0.5028181624971211 -0.0005396605815887358; 0.15264241517349655 0.5627027239358379 0.04026796082311949; -0.21472716598613734 0.5656221884285355 0.07589844603666616; -0.44097859377494264 0.6011415225988948 0.08882761279301371; -0.5596322482349072 0.5924790276186342 0.10349315642725657; -0.6494338922092608 0.5147834423861947 0.09878164045059151; -0.6890853276610861 0.34769944485046655 0.10758903353087095; -0.7017547619444012 -0.20057354620150453 0.09920813690355593; -0.6745685731946026 -0.47742479501621643 0.07312125071193376; -0.6142120609058455 -0.5797834769079339 0.05733530776830226; -0.5194160499914027 -0.6309171109593869 0.04757759512967653; -0.3492605663341956 -0.6402207247189663 0.041146835896067636; -0.03951993531458719 -0.6527963719677305 0.03181129156545075; 0.3274132441095414 -0.6019543607111664 0.027166201765400827; 0.4453849819849971 -0.49234605468138865 0.05074512372671259; 0.5656848679322919 -0.39420475408757977 0.0050941306261821; 0.6326427870763563 -0.00451471603294776 -0.007898661242615889; 0.6344442066851826 0.32653453932748283 -0.009015317754992064; 0.6158812059226126 0.5177117651296143 -0.008708549103931514; 0.2766392824421838 0.6376517469055978 -0.007044397327081956; 0.48635720454238257 0.7015258666642404 0.005391023657919901; 0.2388275095993961 0.7839703160185039 0.0237255785528516; -0.34777254471610497 0.7710290576451031 0.03551844333501986; -0.5885930858213723 0.77414168676162 0.04420044290731061; -0.7164444323934833 0.747056729582095 0.05363112099094788; -0.7783931094123401 0.6945452939195893 0.06286922516715199; -0.8067126938364534 0.5559766275710116 0.07072695146073339; -0.8142556813471 0.18799458490346557 0.08295945452803895; -0.8237609785746686 -0.4171222798419635 0.07484624641818867; -0.7811394140789718 -0.636438184214109 0.06873112603384107; -0.7550230629750426 -0.7150279828307937 0.0684978024408926; -0.6940899011304569 -0.7452234816802559 0.0735184431000053; -0.6007177902464298 -0.7628212138609117 0.08111219954722233; -0.4481244630782517 -0.6927968720256732 0.09187154244235678; -0.18701737720212347 -0.7688281918495833 0.09508018949652022; 0.15330364620088285 -0.7571355696293374 0.10388757294502171; 0.44840462086114785 -0.7349766877868921 0.10468825098380709] %
|
|
Phase 2:
|
|
Planet: Saturn
|
|
V∞_in: [5.478316556422099, 1.2831036594647218, -0.2967788676434742] km/s
|
|
V∞_out: [1.3335401352897827, -2.529320658286065, -2.9636241930342364] km/s
|
|
time of flight: 1.7440266834411675e8 seconds
|
|
arrival date: 2031-02-27T21:22:28.278
|
|
thrust profile: [0.8319809369429529 -0.878794436939913 -0.20832827343669594; 0.8609706878613599 -0.8267238484656785 -0.21318419084570744; 0.8656897434750768 -0.7240384649950173 -0.19979578660603495; 0.8552011838077788 -0.5064814903941824 -0.18251440493384546; 0.8363195973409432 -0.14456572446632004 -0.16593010531881136; 0.8081152165469484 0.18808739340507105 -0.1487369487997654; 0.7768813112799857 0.3321030569792334 -0.13271000839154282; 0.7461547816325443 0.380535079147646 -0.11963434440133103; 0.7336370612568931 0.3876085937165446 -0.11374822501010452; 0.6722438478009509 0.37262354402865455 -0.09924635260998549; 0.636700827451306 0.3482750141362841 -0.09096263174423401; 0.6000979234400551 0.3154896668797045 -0.08347355473204951; 0.565321980717556 0.28197409120639905 -0.07679574071779935; 0.5362347487863641 0.24879840786012403 -0.07052526407699661; 0.506456983388694 0.2178916113871946 -0.06484065560897957; 0.47867392861017327 0.1895873664700829 -0.05934971442801367; 0.45188546802743645 0.16483989816565228 -0.05428532815991076; 0.4258576643452032 0.14314351622849766 -0.049453046387159375; 0.3932180809584342 0.12600938110354004 -0.04515398008512076; 0.3736000015785295 0.1093387430388073 -0.04064878570403887; 0.34746834593741427 0.09663389153595585 -0.03657445916446597; 0.3263804706557932 0.08143119972171763 -0.032253660229846555; 0.29446796677601816 0.07716255241477146 -0.028952185397828487; 0.2675603950018661 0.06913068815160486 -0.025416936036410424; 0.23935147926901057 0.0638464827639863 -0.02232743826164184; 0.2112515499774626 0.058296071404257035 -0.0193898963172417; 0.18154839012996993 0.055479572083340103 -0.016490357086754774; 0.15178288263458828 0.05251212884747476 -0.01386116412051058; 0.12169795930534069 0.049695122256651396 -0.01143496736298545; 0.0910474586010959 0.04765355590466685 -0.009254813498398738; 0.06032007090632702 0.04588860726880914 -0.007296428456263087; 0.024177392897664348 0.055877005503225545 -0.005013775264453432; -0.0013205135851091791 0.04362298856063178 -0.004342404637589318; -0.034268981603339986 0.04171264705427312 -0.003016390318187484; -0.0599598695163209 0.03777860828611642 -0.0011051873513641581; -0.08396131013198456 0.04004076835062581 0.001289908726025911; -0.11237838352227249 0.043118231503448255 0.0038935225675295515; -0.14192940631843057 0.044900767830437484 0.006105003050706572; -0.17249363934725057 0.046526921854485405 0.008060655464185872; -0.2031778124949161 0.04704983155445407 0.00996707335341186] %
|
|
|
|
Mass Used: 1099.5265655762369 kg
|
|
Launch C3: 1.871158167622445 km²/s²
|
|
||V∞_in||: 5.634393045358124 km/s
|