37 lines
20 KiB
Plaintext
37 lines
20 KiB
Plaintext
/home/connor/projects/thesis/archive/best/long_mission---------------------------
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Spacecraft: ingested
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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: 3500.0 kg
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Launch Date: 2023-11-08T16:28:05.002
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Launch V∞: [-4.335012055084635, 4.544887484580865, 0.9951321890482566] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-7.121293324402133, 3.1557449977550442, 0.2574124611969375] km/s
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V∞_out: [-5.88728969114733, 5.091798086780573, 0.4318349867190985] km/s
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time of flight: 7.69225867524608e7 seconds
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arrival date: 2026-04-16T23:51:11.002
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thrust profile: [-0.03956033280289971 0.014502274153396886 0.013767483820172557; -0.041576479761307766 0.010774744221230172 0.015954618100526122; -0.04353519609600167 0.007026291842675089 0.018015518823847464; -0.04547258505717467 0.0030483408188381605 0.01993777253806961; -0.047309011488274606 -0.0012193548498561485 0.021657327331670945; -0.052415487659225525 -0.06416407139171071 0.01707388662648066; -0.053795860137490825 -0.06910602876361567 0.018377866968160055; -0.05478537648848572 -0.07435827994314907 0.01948872251679001; -0.05534637430302962 -0.07987969781686377 0.020391393740754694; -0.05542234511951779 -0.08557119998417642 0.02112165287536681; -0.04603653494469639 -0.11758339178872364 0.010478731803032337; -0.045131078072944794 -0.12330822437476184 0.010879231121188585; -0.04374974899764054 -0.12899509823771538 0.011155318621208977; -0.04192900589988677 -0.1345812372404263 0.011297583377631603; -0.039688700024628897 -0.1399961637348015 0.011314220390491788; -0.021847974947327285 -0.16435052102367306 0.002129770511850757; 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0.30810889360138993 0.10225487688815191 -0.025340625186851942; 0.3046520673782745 0.1111657055432318 -0.02519931087775893; 0.3006841235275496 0.12016917200239183 -0.024980281657263303; 0.2961738618627909 0.1292489694856472 -0.024701968974558373; 0.2735165965939293 0.1619979905410212 -0.01869630655188906; 0.2676587760768934 0.1710598613565007 -0.018258442297774177; 0.2611268574754945 0.18010472448692472 -0.017743059114779546; 0.2538542304726611 0.18910841101106657 -0.01712960149634353; 0.24581028537105218 0.19800484453654849 -0.016418319274889952; 0.20666869884086048 0.24449798918762772 -0.010479404541833484; 0.19661838861414238 0.25278629475126474 -0.009583933716756832; 0.185593310022131 0.26078424163575775 -0.008578297521869437; 0.1735491928214268 0.2684089062735019 -0.007463828245551458; 0.1604241654210947 0.2755419168542371 -0.006243673883006362; 0.11764420987192885 0.3026128805297053 -0.0027808955696240526; 0.1020256537979734 0.30819300429344426 -0.0013314690854612414; 0.08524068300499618 0.31284158307591525 0.0002381332205356246; 0.06730138419613374 0.3163648963620088 0.0019230866854307947; 0.04826513140941637 0.3185318511746061 0.003707513869349553] %
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Phase 2:
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Planet: Jupiter
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V∞_in: [-2.4700745323840945, 3.5992843576814684, -0.04897910356619292] km/s
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V∞_out: [2.3726396804033665, 3.660071493225041, -0.18342240674607424] km/s
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time of flight: 1.0365627669349752e8 seconds
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arrival date: 2029-07-29T17:15:47.002
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thrust profile: [-0.05988472231417988 0.5098718574120789 0.003380381450714991; -0.09985679108378966 0.5099970456619252 0.007680524392304216; -0.14083421951474379 0.5051230227055744 0.012059671089214113; -0.1806537704798288 0.49506022146586576 0.01638507392002354; -0.21707969492739523 0.48021220494730227 0.02057113683022605; -0.32471394771469786 0.4295719891811384 0.01872201874781426; -0.347149092726571 0.4026010250742786 0.022369089660714277; -0.3635390170080211 0.37415292304681513 0.025671314432171383; -0.3742393760147842 0.3457764845105525 0.02865266479348716; -0.3800621096770123 0.31860555955757813 0.031325752410159356; -0.39269541135392216 0.2188962027151091 0.03258569777778156; -0.39145308216679325 0.1937691388951771 0.03471143696114105; -0.3880119345885402 0.171349220288765 0.03661393416731571; -0.3830191997329326 0.15157634467357106 0.03831373113348574; -0.3769823877981445 0.13425557848329225 0.039836235108387456; -0.35514383707999975 0.0942343336397406 0.04952161544225744; -0.3477490228181278 0.08104440223464975 0.050723794597789085; 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0.013653698635247962 -0.010768062445170068 -0.0035421759772075873; 0.014850558635080485 -0.010407794132715763 -0.004501417594322374] %
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Phase 3:
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Planet: Saturn
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V∞_in: [-1.288181310839508, 3.2263876606130104, -0.15259601195389053] km/s
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V∞_out: [0.48748673373831564, 0.4905484443382068, 0.477662291276709] km/s
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time of flight: 2.643066332108945e8 seconds
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arrival date: 2037-12-13T19:46:20.002
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thrust profile: [0.05787434800100662 0.06365972987059527 -0.004690937847485817; 0.058804962259307765 0.0631535995879651 -0.004740314009454671; 0.05983542454257423 0.06268609928169047 -0.004788047127416414; 0.060975433718026835 0.062268789932902475 -0.004835524503135446; 0.062225980024771796 0.06191324474149255 -0.004880865078012681; 0.06285801042135475 0.054884663480775316 -0.004819160140313061; 0.06433749312618502 0.054701052047457566 -0.004861768137879246; 0.06593351900262197 0.05462711861876099 -0.004903833691377991; 0.06764791684805822 0.05468390798107871 -0.004945075327582575; 0.06947857183941591 0.05489653022456621 -0.004980756541231241; 0.07158131197912566 0.05370903624290616 -0.004989096177551872; 0.07363165632802447 0.05431132268456726 -0.005020718083045292; 0.07577820988565821 0.05515538438056131 -0.005046798453303127; 0.0780073675020361 0.05627588650036708 -0.005067760214972139; 0.08029568923374143 0.05771722861801827 -0.005083195330091614; 0.08641404640859522 0.06540989432376075 -0.005159860038250109; 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-0.02127206654031124 -0.01567617264428185 -0.002793411190767065; -0.02022956859236421 -0.0159188548014709 -0.0028738271376681866; -0.01918789336871752 -0.016160901736099867 -0.002954272690873852; -0.018146303148503164 -0.016402883837149045 -0.003034785707982439] %
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Mass Used: 530.668253715296 kg
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Launch C3: 40.43861983890888 km²/s²
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||V∞_in||: 3.4773947099827938 km/s
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