23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5999195459953728---------------------------
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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: 2023-04-19T11:09:39.273
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Launch V∞: [5.201284225210998, -8.186736204551094, -0.2639699750216843] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-0.1349450071639801, -0.18872283693609418, 0.03038190878795008] km/s
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V∞_out: [-0.2959000471764254, 0.029400282801974598, -0.015437619169804408] km/s
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time of flight: 1.3109040059244588e8 seconds
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arrival date: 2027-06-14T17:09:39.273
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thrust profile: [0.7287314574151093 -0.4517553071898804 -0.28436595205371107; 0.36120862081088406 -0.023029087893686167 -0.31569983184708267; 0.12874006774113705 0.01979519098736216 -0.17650380531189722; 0.1662535049684736 0.049154563388085035 -0.28748102216228855; 0.15580854611549366 0.06497951202916129 -0.3238726069171766; 0.06916553576527146 0.03050589089797591 -0.16958548949252372; 0.0549767303572832 0.026692308628690476 -0.1500999197265713; 0.02088748545111169 0.009590025928177353 -0.058107673993874155; 0.0032246824167098606 0.0009495843507505665 -0.0020892198649673176; 0.0073162147507302225 0.004407590242239905 -0.019150459714172507; -0.006916079165807197 -0.0018557425603812883 -0.013137761561594973; 0.007402931753700963 0.004748285869200413 -0.009961106764701603; -0.005029695646667741 -0.002189152519558534 0.004789361678981986; 0.0015626130737990192 0.0015819050393360385 -0.00594123436167719; 0.004671887817688136 0.020949486602003235 0.003358293500773887; 0.003788487420142364 -0.02273962687527002 -0.005599813939054729; -0.0053087079677953996 0.0171488549681535 -0.014375857553156863; 0.013423110031930028 -0.008966813343613936 0.011249577763232438; -0.00711612132345568 0.0027337383911758507 0.00910055692072655; 0.006063110369797149 0.0024565254908954027 -0.00013225201010168253] %
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Mass Used: 150.72296036598027 kg
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Launch C3: 94.14568742204936 km²/s²
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||V∞_in||: 0.23398616309793527 km/s
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