30 lines
3.4 KiB
Plaintext
30 lines
3.4 KiB
Plaintext
/home/connor/projects/thesis/archive/EMS_2021-12-12T15:39:06.197/mission---------------------------
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Spacecraft: mySat
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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: 2023-04-04T08:15:42.979
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Launch V∞: [4.591627441054104, -0.9372602729162841, -1.402102560672615] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [9.367085838054193, 1.2385416703463588, -1.2664210112872778] km/s
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V∞_out: [9.488354168340724, -0.7139124540608336, -0.5849794139568701] km/s
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time of flight: 2.4606079841224298e8 seconds
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arrival date: 2031-01-20T06:29:00.979
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thrust profile: [0.48110193115514666 0.1658344957098272 0.18875138957299367; 0.2722197721770649 0.41958962982537107 0.2031126777241352; -0.14912794861230844 0.31014754435480146 0.20231048078147726; 0.41900792223774436 0.33923945509259673 -0.3410850527690159; 0.2511755140919902 0.5014702815333173 0.0058685456880530696; -0.15486070913892752 0.2360830420399679 0.2645880501135092; 0.225939307553581 0.3555635470518182 -0.2579478714227079; 0.4692868559854733 0.36449584745921737 -0.26361975800532383; 0.17776955473214556 0.5344512134705717 0.2677028115850273; 0.29341528211428775 0.25652205797659977 -0.003223292822703167; 0.47969842043937694 0.383501318717164 0.00793282457827181; 0.0557455430628551 0.42410040402941707 0.12847485289641172; 0.42501735100730476 0.4434488658095193 0.17406200336317385; 0.2586191172669515 0.3545965771776789 0.13169086497478733; 0.3994448644962761 0.3523601532459076 0.1980455999347843; 0.2712389420869066 0.2551872658044702 0.16820587889445787; 0.7160832227791448 0.05007832921773097 0.03084211842871704; -0.4014048218424198 0.4263176448200758 0.02349504793730896; -0.4648045356639775 -0.012165497397007176 0.07112680698673901; 0.3334382990840683 -0.6819542566923011 -0.05838594675754101] %
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Phase 2:
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Planet: Saturn
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V∞_in: [-3.033179205299309, 8.323540792555027, -0.834135394854228] km/s
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V∞_out: [-1.7989044724374927, 4.992471036908333, 2.7395017565836506] km/s
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time of flight: 1.343904325951288e8 seconds
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arrival date: 2035-04-24T17:09:32.979
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thrust profile: [0.7399454327526205 -0.5303156843529576 -0.01303320908827589; 0.8546930606858686 0.056047121557869325 0.01672326772293818; 0.8757001417012732 0.8092300745166227 0.08014191465251598; 0.7798406512457665 0.8508819508472818 0.0649883040365693; -0.03926761644682386 0.8522354272278931 0.027089526497775643; -0.434264020033893 0.8459075469832358 -0.0040464336106154335; -0.5548067523933243 0.8328498997908219 -0.030544100084358417; -0.5947401029696081 0.8138198308943535 -0.049034191658682065; -0.6075585777480846 0.7820903525414267 -0.062173373203187395; -0.6029505069844785 0.7335072879202299 -0.07007906442079202; -0.5799580021535939 0.6730106758444432 -0.07459794494237851; -0.5482338658185978 0.5906864307437136 -0.0756851978219243; -0.503124125207766 0.4976084605014916 -0.07059787047969154; -0.4525092012219953 0.3942979609123233 -0.06424348023914521; -0.39298962065606696 0.2862145343873863 -0.055308865576020064; -0.3253259710648706 0.17741161874473715 -0.04466835734562229; -0.2605713062487545 0.07474580225090127 -0.03489801748303663; -0.18829323187093158 -0.02019200756889348 -0.029721867673255048; -0.12407983907216594 -0.09176887331289074 -0.014975937367657555; -0.07399819648159202 -0.17898421972733056 -0.0006361521051712036] %
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Mass Used: 1847.197572706729 kg
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Launch C3: 23.92739096727287 km²/s²
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||V∞_in||: 8.89816212898688 km/s
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