23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.7290074656059045---------------------------
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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: 2024-04-27T03:12:19.009
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Launch V∞: [8.279562153476801, -6.749228015343227, -2.0999360279881847] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [2.2762264600732687e-7, 1.7138249725056731e-6, -3.612442046057855e-5] km/s
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V∞_out: [-1.3522936621672475e-6, 3.610796875002602e-5, -3.705016850033932e-7] km/s
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time of flight: 9.139968729907428e7 seconds
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arrival date: 2027-03-21T00:00:26.009
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thrust profile: [1.0 -0.5753303639166572 -0.4498231853763222; 1.0 0.037863518223634055 -0.6450579187720803; 0.7314571469533068 0.1943521428776876 -0.5118329705511118; 0.41378977623601915 0.1705894913490041 -0.35898101379279806; 0.10300522894235381 0.0538033938569479 -0.10586104148805744; 0.06427989226126234 0.038359180221615816 -0.07386256068149047; 0.010878168707596088 0.00797630971972508 -0.014081245549867363; 0.005185097581346366 0.00015047409637881232 -0.003645899944708283; 0.002754754536311115 4.5831135903925783e-5 -0.0031832679972535055; -0.005766104178953708 0.0009805998312201157 -0.002922410083877368; -0.004892844297811089 -0.0034940521899910065 0.003103192523420559; -0.009323947629692105 -0.0033898647810544887 -0.006677921349901767; 0.014112231121937735 0.0007252895868020588 -0.004464979916574685; -0.002131243080615324 0.0003021174636728579 -0.00014579280468561637; -0.0001447578285185304 0.003568853233389526 -0.014056609287059795; -8.664798203153815e-5 0.0009896238522672412 -0.00026236522564656185; 0.015273488035635222 0.00964407244526353 0.014940215868120235; 0.02273005060842498 0.01900239693094135 0.003520075962942629; 0.02950926877567977 0.0033254606796539916 -0.005706709435462306; 0.021781906019182045 -0.004627892814737714 0.008482080773125792] %
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Mass Used: 159.18311233509303 kg
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Launch C3: 118.51295957802208 km²/s²
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||V∞_in||: 3.6165767815961355e-5 km/s
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