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thesis/archive/EMS_0.956419624778337
2022-04-18 10:59:25 -06:00

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archive/EMS_0.956419624778337---------------------------
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: 2024-09-17T04:51:36.159
Launch V∞: [-1.135592828872187, 4.562737698529162, 1.3727576611586305] km/s
Phase 1:
Planet: Mars
V∞_in: [-3.557470090326179, 6.118653602166694, -0.5798401682157046] km/s
V∞_out: [-5.645943535485121, 4.274383608710339, -0.5316919206121211] km/s
time of flight: 1.3085999999776801e8 seconds
arrival date: 2028-11-09T18:51:35.159
thrust profile: [-0.09484105234506424 0.13109265638731943 0.010936530688181876; -0.1814554654952118 -0.01317670830456729 -0.013056779511401079; -0.03810385790137717 -0.03831609614699233 -0.0090400245120533; -0.011547804227375344 -0.045340160916842225 -0.010789638825569993; 0.010850150398340981 -0.04880193320022692 -0.012185437423926783; 0.013978839278259155 -0.01840779353950528 -0.004665802971635902; 0.015830676636944672 -0.006108261481050007 -0.001974030494045432; 0.02222629553617521 0.007131223648098273 -0.000366596741242515; 0.05551908016805829 0.2775937664715688 0.01624399186055875; -0.11493741715972325 0.07648127820140446 0.005075332093053433; -0.07281410027212154 -0.023271489715626266 -0.00280576336716608; -0.03991641354611127 -0.052482033366050736 -0.012070494591368944; -0.010823677700697571 -0.06926247781385951 -0.014965378527982062; 0.014553072546870926 -0.0531151232441876 -0.012334544418377249; 0.027433879698947325 -0.03222960647822717 -0.008091377392690582; 0.027896088095082885 -0.010765686776681731 -0.0035677146904594865; 0.1474887355876181 0.04194010217566325 0.0075472784087007245; 0.08740136907489779 0.2476740961050621 0.025348796622511757; -0.3587107107731137 0.3658303122853691 -0.024033216941170596; -0.30793493577932085 -0.02489759271709177 -0.029516702132738652] %
Phase 2:
Planet: Saturn
V∞_in: [3.7155109082507987, 4.436831582591491, -1.1732520095761172] km/s
V∞_out: [-2.9774108815083147, -1.2560337688716137, -4.9297276650048545] km/s
time of flight: 2.0467080000004956e8 seconds
arrival date: 2035-05-06T15:51:35.159
thrust profile: [-0.05767594934959341 -0.04617371221776187 -0.0018460762847027803; -0.00242135160333423 -0.04166237973886581 0.0014630203665685387; 0.29042498349326934 -0.4463318141243284 0.034252710040742367; 0.9999918983032768 -0.6810996795092573 0.08973482264944235; 0.999994193014499 -0.30520092641941937 0.09457239144251212; 0.9999870255556219 0.2194024540716046 0.09015740448455901; 0.9999831603785917 0.9750561249047252 0.0872456396613651; 0.9999985694625713 0.9999931657134729 0.05615632466445174; 0.687392266640871 0.9999956716419007 0.01734725859208972; 0.029368471497984026 0.99992751557616 -0.014405154294501676; -0.20296396601376304 0.9423006803678043 -0.03524904229410645; -0.12775237609043735 0.3694446313295914 -0.02368746549915993; -0.00034842736779606184 0.0005678692895095884 -0.00031598317940006337; -0.0003712455053865169 -1.6935819288267125e-5 -0.00019252189104459086; -0.0005996017322677676 -0.00028098465395757154 2.2184451692068863e-5; 0.0002022591204715913 -0.00018951661125293372 0.000189711737865895; -0.0007251432775536019 0.0002897166773871866 -3.9173461655229126e-5; -0.000850251276017041 -0.0005646508814492377 0.0013737659604325715; 0.00040972949658941917 -0.0005145490913947212 5.515738964126715e-5; -0.00046082039982410966 -0.0003000114452015229 -0.00026022069154713355] %
Mass Used: 975.8660040548566 kg
Launch C3: 23.992609974834842 km²/s²
||V∞_in||: 5.9048298942125665 km/s