23 lines
1.9 KiB
Plaintext
23 lines
1.9 KiB
Plaintext
archive/ES_0.723051144570667---------------------------
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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: 2024-05-07T08:42:47.895
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Launch V∞: [7.152828094911789, -7.414899147873033, -2.1172460958801302] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-0.20558537518394945, 0.16954560632397586, 0.0215637450111708] km/s
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V∞_out: [-0.1728213558155897, 0.1379076599366388, -0.15022312518061437] km/s
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time of flight: 1.0372837990344004e8 seconds
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arrival date: 2027-08-20T22:09:06.895
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thrust profile: [0.8080585976821513 -0.4042799480341829 -0.43096014816121514; 0.39968135767513896 -0.018848765328998988 -0.3845954780405658; 0.16980409815662623 0.02797903125923218 -0.2228063303348119; 0.09627125407858557 0.030565764269643733 -0.1484335484302719; 0.02587667605258764 0.014043026119807483 -0.042025050115259976; 0.009479549982496432 0.008227307790088376 -0.015701514199754945; 0.09857787906649734 -0.02161776899242402 0.007817732000153614; 0.0035159364957274408 0.028370353692004253 -0.018375527593470643; -0.03415599218499986 0.007607216055770306 0.03491561445024274; 0.010347892577004213 0.0061738258846286065 -0.05407161676994101; 0.08574390178549834 -0.030755545540481363 -0.09151190161138907; -0.04500495651875149 0.03359578439823552 -0.006318117103527853; -0.01791125816004757 0.0031958895128004813 0.061014976176691035; -0.044929329518973625 0.31553910639772426 -0.06080433498839516; -0.060332243619076624 -0.3147284480436024 -0.22535556017699798; -0.018679919381674123 -0.010880090452072848 -0.029100830483129985; -0.10059504397131147 -0.24913509315277363 -0.1558693490385519; -0.06435582494025434 -0.019836933350007815 -0.3433393425817294; -0.3679767021029245 -0.0439568776960443 0.3458042364930179; 0.10077026659881971 -0.05099597243598219 0.27988144072783144] %
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Mass Used: 198.23894273823544 kg
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Launch C3: 110.6264101590073 km²/s²
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||V∞_in||: 0.2673500593083844 km/s
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