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thesis/archive/EN_2021-10-14T23:27:47/mission
2021-12-13 22:23:31 -07:00

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archive/EN_2021-10-14T23:27:47/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: 2022-10-01T14:30:44.231
Launch V∞: [-1.5243188475966056, 5.9256671205622045, 0.2916154666540272] km/s
Phase 1:
Planet: Neptune
V∞_in: [3.6975966998821526, -1.4215737222278524, 0.3088257373177974] km/s
V∞_out: [3.445686587806444, 0.6826200114085932, -1.001538192708208] km/s
time of flight: 2.855355071164953e8 seconds
arrival date: 2031-10-19T09:55:51.231
thrust profile: [-0.8759933715507354 0.9721696493713093 -0.019442309148699335; -0.8008537600952194 -0.5941302460728478 -0.06796587793610398; -0.627589785584642 -0.8318706537968823 -0.08563284635359299; -0.840841194502072 -0.9445735606822884 -0.0955284075050304; -0.3600239078894093 -0.47204355869564657 -0.11126127685731058; -0.7388484282650255 -0.7886435929888026 -0.08909986800032511; -0.32305894084141484 -0.30591569708824085 -0.10340952135470989; -0.28216239907675256 -0.1426792583554665 -0.1143226817898616; -0.09639141414540019 -0.011528842076150791 -0.26755240273453423; 0.18814683852103375 0.4893924983795105 -0.04759899728071763; 0.31623329829219116 0.48035347011008334 0.021140757522982417; 0.3495977355479997 0.48970181862122203 0.050702499356316995; 0.35078134471647493 0.5710967629548804 0.08085199199019613; 0.4242295692725758 0.6648754488413917 0.11708559827741634; 0.7544685450994223 0.6138555082590391 0.1547920784756316; 0.3078505072984024 0.6964463042108037 0.17903196782627837; -0.3363787766756175 0.3963963385214657 0.06482748384126795; -0.33655861967802553 0.3496684000706546 0.08953707892324089; -0.18529532214490396 0.27841610852846016 0.04136003156954945; -0.013754111231380713 0.1364854049755323 -0.023729392781819306] %
Mass Used: 1572.0861495426557 kg
Launch C3: 37.52211835324206 km²/s²
||V∞_in||: 3.9734703394813478 km/s