23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/EV_2021-10-14T13:48:25.788/mission---------------------------
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Spacecraft: mySat
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dry_mass: 2000.0 kg
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specific impulse: 3200.0 kg/s
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max_thrust: 0.0005 kN
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num_thrusters: 2
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duty_cycle: 1.0
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Launch Mass: 4000.0 kg
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Launch Date: 2022-03-03T16:03:54.308
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Launch V∞: [3.1331875390553874, 4.743765316753105, -0.6321137349156039] km/s
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Phase 1:
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Planet: Venus
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V∞_in: [0.7336287799525429, 9.092380028023765, -2.060897868194347] km/s
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V∞_out: [-0.005397228824250161, -6.841249447820443, 3.86835501811607e-7] km/s
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time of flight: 1.431136134384693e7 seconds
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arrival date: 2022-08-16T07:26:35.308
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thrust profile: [-0.029700857947171155 0.037677806973394956 -0.0016513225652095235; -0.09203896237700117 0.06668008002755799 -0.003907365708797221; -0.15385799693549973 0.09456424369948617 -0.00567508250690443; -0.19644155536268554 0.12045167230584422 -0.010220562279956805; -0.28443665959408854 0.13387251178059187 -0.010826054663009434; -0.35314485464965406 0.1508209960737375 -0.014312066894957601; -0.42349740669156993 0.15073261096749926 -0.01617441359738227; -0.49179611760767494 0.1313289360663566 -0.019420534802667432; -0.5498265630622056 0.07689683044740066 -0.022535038089659315; -0.5841007485384517 -0.028343225924705343 -0.025645308771199683; -0.6463113947204338 -0.19361054238923944 -0.030545065432850942; -0.7020011201668798 -0.3987157016634757 -0.035892266940698137; -0.660261751730148 -0.564813684339657 -0.03928441369489666; -0.5533792180410886 -0.6697142859509423 -0.039751339872136054; -0.35878759946251465 -0.6287274757834188 -0.03432166295686523; -0.07897641529965045 -0.6890633639101433 -0.024417495241929963; 0.1132061820810732 -0.5814939033233674 -0.011948487492265437; 0.1525591439015402 -0.4915765280189982 -0.0025092936276034316; 0.10348417965356019 -0.4089525878329189 0.0030668463178562854; 0.024035973004629382 -0.3568182136414068 0.0051715969680988395] %
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Mass Used: 225.67816334678992 kg
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Launch C3: 32.719741309190596 km²/s²
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||V∞_in||: 9.351838631194836 km/s
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