30 lines
3.4 KiB
Plaintext
30 lines
3.4 KiB
Plaintext
missions/nlp_2_phase---------------------------
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Spacecraft: bepi
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dry_mass: 2000.0 kg
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specific impulse: 2800.0 kg/s
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max_thrust: 0.0005 kN
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num_thrusters: 2
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duty_cycle: 0.9
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Launch Mass: 3600.0 kg
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Launch Date: 2021-10-31T23:59:59.740
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Launch V∞: [1.0519139174671255, -2.532396776578504, -2.3181056242189095] km/s
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Phase 1:
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Planet: Venus
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V∞_in: [0.4221053576448278, -3.5275571377673485, 4.891092995284791] km/s
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V∞_out: [2.663171797047433, -4.912541295851552, 2.3063442275330837] km/s
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time of flight: 1.2614399648580924e7 seconds
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arrival date: 2022-03-26T23:59:58.740
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thrust profile: [0.07998955511503905 0.014645901175208607 0.032059542365265536; 0.061271963308267355 0.010496084457312739 0.06456227213436845; 0.03653858968490382 0.004095269984271039 0.08778809213169904; 0.012597606226571892 -0.0035843497513941024 0.10156429358711754; -0.007823696996985706 -0.012212563689391798 0.1092387978999297; -0.024470397395360978 -0.022164965343914263 0.11328387576041525; -0.03764018531138568 -0.03305106575614711 0.11485841832796724; -0.046956531921797474 -0.04462741732738438 0.1147527426828988; -0.052986295209290435 -0.056908842131396964 0.11331606017641183; -0.05501214840088177 -0.0698229298399496 0.11102391517980509; -0.0539274775951607 -0.08225923304281293 0.1080571865577752; -0.04900248855811753 -0.09498380663479362 0.10399629481809765; -0.040344197913873656 -0.10681215838405833 0.09912867572917736; -0.028118935327375093 -0.11715254048024237 0.09312311669260512; -0.012343877715426374 -0.12544654901191046 0.08544366039001013; 0.006110502843051679 -0.1305027433772816 0.07629177701281903; 0.026362754169644998 -0.13201279652190237 0.06480681138449274; 0.046333885834596335 -0.129332099528906 0.05156965147459962; 0.06457348912678001 -0.12274635759961078 0.036509818421423236; 0.07952353937438418 -0.11313097843352427 0.019798449229470383] %
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Phase 2:
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Planet: Mars
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V∞_in: [3.880922081076609, -3.8756380279560982, -1.179545632109947] km/s
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V∞_out: [-0.006991844594378784, 0.007675557473077985, 0.0017824029323501372] km/s
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time of flight: 1.330560006563769e7 seconds
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arrival date: 2022-08-27T23:59:58.740
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thrust profile: [0.12305856757522188 -0.14464704712095547 -0.01690236351704525; 0.13429815673794188 -0.1195285218500703 -0.023483980378131736; 0.1396586011579744 -0.09516174490601491 -0.0293944316107087; 0.1405117586368446 -0.07304441529598331 -0.03420656443020225; 0.13837132835970684 -0.05371429903466249 -0.03776391678703145; 0.13446436956407476 -0.03753581708426115 -0.04027955684165351; 0.12971675491549636 -0.02368494568417238 -0.041313837916754456; 0.12476791885955194 -0.011918609837526017 -0.04089459243732129; 0.11990410375769957 -0.0013599111496390207 -0.039013892415853124; 0.11535184137947554 0.008625420550911504 -0.03547549318320644; 0.11060362891923352 0.01858862039347281 -0.03026382720393468; 0.1051121620536058 0.02900798484914558 -0.02356021862070372; 0.09847113469008412 0.040066844453614206 -0.014965931800162527; 0.08971089782921067 0.051422184661349964 -0.005111452945431483; 0.07802582953613077 0.06259376060544532 0.0051850295654957725; 0.06311411546227669 0.07276616262027279 0.015795273832386957; 0.04546470094052957 0.08070053397671015 0.025466309765173768; 0.026472095432748317 0.08567894187220633 0.03355591354621125; 0.006854607387209108 0.08788158299954184 0.03976962429050834; -0.011956529938837489 0.08738091721577941 0.04450602440724739] %
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Mass Used: 121.82108539595492 kg
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Launch C3: 12.893170008821572 km²/s²
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||V∞_in||: 5.6101206957923 km/s
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