23 lines
2.1 KiB
Plaintext
23 lines
2.1 KiB
Plaintext
/home/connor/projects/thesis/archive/EM_2022-03-29T21:30:57.022/mission---------------------------
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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: 2024-10-12T01:36:00.330
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Launch V∞: [-0.34441487078455013, 3.9103321083115397, 2.032019563693426] km/s
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Phase 1:
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Planet: Mars
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V∞_in: [-1.323280834421365e-9, -1.305249079827022e-9, -1.756498248174488e-9] km/s
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V∞_out: [-2.072434338771005e-9, 3.1188692292717017e-10, -9.96060247089551e-10] km/s
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time of flight: 1.9187428749374934e7 seconds
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arrival date: 2025-05-22T03:26:28.330
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thrust profile: [-0.0006647023892816537 0.004035322252316528 0.002450694309122812; -0.0010810936123367345 0.0033648421104130093 0.003041727879478422; -0.0013507121101609906 0.0028319436906776322 0.003294754033895274; -0.0013817337282281677 0.002283246633035519 0.003911472841560675; -0.0014099790469406482 0.0016622747910402052 0.004243346099566735; -0.0012603732201070137 0.0013617718291820912 0.004609732990326976; -0.001109687893062513 0.0010166792245012248 0.005257291391887101; -0.0009765487656423202 0.0007701050283466614 0.0045962916304727545; -0.0008511110507625 0.0005562454707099463 0.004264167411226241; -0.0007373982279473773 0.00044288704744547956 0.0042335052666390175; -0.0005724074417038922 0.0002590516109966243 0.003593127587839534; -0.00048097983471947337 0.00027784548514532824 0.0036573739539471012; -0.0004010082145124844 0.00023837273061184575 0.00295844216959782; -0.00030319886238157107 0.000188351968848797 0.0026590665546669954; -0.00013453010791864773 0.00015049323913512056 0.002533970064140107; -0.00017918516868998714 0.00011876509991415298 0.0020961759015662375; -0.0001309746244392474 9.400293297511669e-5 0.0016359370993405285; -8.735433670043718e-5 6.50059985134959e-5 0.0011999019334906667; -5.205594667799379e-5 3.959950287622984e-5 0.0007255745258836434; -1.69083877031164e-5 1.3250954732018612e-5 0.0002522304876801491] %
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Mass Used: 0.5263628244356369 kg
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Launch C3: 19.53842230774253 km²/s²
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||V∞_in||: 2.5573489052095017e-9 km/s
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