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thesis/archive/ES_1.8019411464307387
2022-04-18 10:59:25 -06:00

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archive/ES_1.8019411464307387---------------------------
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: 2024-03-21T16:46:01.450
Launch V∞: [9.58656184545047, -3.970937169707667, 2.2063087746538907] km/s
Phase 1:
Planet: Saturn
V∞_in: [3.6303953820160487e-6, -0.00023853624892790178, -4.178248371415312e-6] km/s
V∞_out: [-0.00022366317941333277, 3.3931931633146954e-5, -5.259478273676722e-5] km/s
time of flight: 1.874957778810701e8 seconds
arrival date: 2030-02-28T18:55:38.450
thrust profile: [0.8402152736723273 -0.2691465875016191 -0.051376898789932464; 0.8260983236486968 0.6274716097728676 0.0604898877854466; 0.8096946258627372 0.6297857774248286 0.10431390343765866; 0.840846116974009 0.3992699151287581 0.07729078662824075; 0.8634105774350551 0.12174968062600099 0.09717565222506726; 0.8581567074976978 0.02264269016479872 0.09431742567924492; 0.827267087668885 -0.5119322420274552 0.10000296623403016; 0.7336156578060631 -0.7868028288743042 0.0656798470276993; 0.5157024811482248 -0.8880530682492028 0.05009160261235823; 0.445328141100846 -0.9542008185700589 0.08888443983391493; 0.9704964740606297 -0.958713862483643 -0.006032213505754519; 0.9439720683009278 0.9523064245570626 -0.17105490425415132; 0.9074332073163462 0.9288172875357916 -0.07713635722793118; 0.8663255936770708 0.06319609750396514 0.10261595976772894; 0.373061236716911 0.16527228836583324 0.22700787202283618; 0.8684331726664528 0.8804772915523542 -0.02570976814762694; 0.7252888497461953 0.8499784091749091 -0.011832978706627076; 0.5194476430411283 0.7815326545806969 0.0024255093126412594; 0.29239675001367055 0.628796684312392 -0.006225365913084095; 0.10458348166315978 0.22815559743849018 0.0006608641105584641] %
Mass Used: 1445.7912049852853 kg
Launch C3: 112.53830843152741 km²/s²
||V∞_in||: 0.00023860046014766384 km/s