30 lines
3.4 KiB
Plaintext
30 lines
3.4 KiB
Plaintext
archive/EMS_1.7849375588806782---------------------------
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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: 2024-12-27T01:12:40.730
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Launch V∞: [1.8466699553948345, 1.3678562790010131, -0.0153057964937058] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-3.1633872892711388, 1.766847714739104, 1.5906318484460866] km/s
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V∞_out: [-2.6570752417451518, -1.5623087854586397, 2.48153623885944] km/s
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time of flight: 1.3537387772095194e8 seconds
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arrival date: 2029-04-11T21:03:57.730
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thrust profile: [0.9929900810043344 0.9999987852496462 -0.10337727636552446; -0.9999989527606722 0.9999992090099894 -0.3047289804175132; -0.9638713659439484 0.0450322438551014 -0.4055337795064804; -0.22495106561402115 0.7848677069324818 0.3831319023782979; -0.7738893421351393 0.9999990172621287 0.39494769205095726; -0.990946731002965 0.8417897053927665 -0.3815221486365675; -0.9734982361035388 0.7893313668448306 -0.2704704369660258; -0.38723803350107505 0.9976585911266805 0.3624717872401706; -0.6369591805380839 0.9888790443583878 0.2130500370042681; -0.9999988687936101 0.9999990044599046 -0.3329147869188805; -0.5789162319974664 0.1999123448513483 0.028083803862645515; 0.7985291692991425 0.7881953295377477 0.17388971281195142; 0.988850032987504 0.9999996591217118 -0.5009694317683372; -0.9999994842664317 -0.3956604351616602 0.20708177708047873; -0.4450447334188467 -0.9872965011676511 0.25277979453414506; 0.9999992382496556 -0.2261999230664443 0.0610408161667454; 0.9999995915291495 0.9999997964336237 -0.5276666165499095; -0.9999998232725931 0.9999996435539122 -0.2721356921234991; -0.9999996876222519 -0.99999900073252 0.10007758955670606; -0.4315629068159034 -0.9999994920612009 0.07571074821215397] %
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Phase 2:
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Planet: Saturn
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V∞_in: [1.327202961748595, -0.2335174765716992, 0.19517799010581816] km/s
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V∞_out: [-0.10390899330694657, 0.5823202662968701, -1.2235226316464973] km/s
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time of flight: 1.315170240574828e8 seconds
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arrival date: 2033-06-12T01:34:21.730
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thrust profile: [0.9999991434090886 -0.9999989109820826 -0.18840484920575698; 0.999999642574456 -0.7892776436332918 -0.12931408694138657; 0.9999997178412163 0.5267393788441906 -0.06956780561709845; 0.9999997101961674 0.9999994336962261 -0.018610639490947056; 0.9999995326675502 0.9999996674548184 0.04055505772364419; 0.9999985272401802 0.9999997166093685 0.0964843343858098; 0.5108611241098074 0.9999996665528476 0.11541241396889583; 0.11915209802429379 0.9999995788468198 0.1254892030062545; -0.06577608027600101 0.9999995097151354 0.1358163701800956; -0.15786944384121993 0.9999996754541017 0.1375960485939181; -0.19165177643017128 0.9999893885682953 0.12875243461837188; -0.1283595672922781 0.6138567630147376 0.07671724293817712; -0.012317449010467607 0.047087977571726294 0.006452581509892722; -6.34335149466746e-5 0.00091471809306928 8.53716230858717e-5; -0.0002753957972021203 0.0008379366569403406 0.000253847549893273; -0.00012249698733454806 0.000620864691591944 0.0001747719954028129; -0.0007703906582188425 0.00036864647470518063 -0.00026313495806057455; -0.0003679676279671012 0.000462432306598997 -0.0005969365300740931; 0.00010307940670236174 6.503004811360405e-5 0.00016002455788454703; 5.626567684290205e-5 0.00028538089451470705 0.0003865580217838497] %
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Mass Used: 2051.6186645766516 kg
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Launch C3: 5.281454991566764 km²/s²
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||V∞_in||: 1.3616506752322357 km/s
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