23 lines
1.9 KiB
Plaintext
23 lines
1.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EJ_2021-11-10T17:36:57.486/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: 1977-09-23T03:22:48.372
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Launch V∞: [-9.493171911757265, 1.996521857385693, 1.8459560902623946] km/s
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Phase 1:
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Planet: Jupiter
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V∞_in: [-9.543974938238337, -5.087831983949424, -0.35708404363703494] km/s
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V∞_out: [-0.129298458647144, 0.15324446409210052, -0.009200490470804264] km/s
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time of flight: 1.776357220782331e8 seconds
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arrival date: 1983-05-11T02:38:10.372
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thrust profile: [-0.7610489826673982 0.4519575670810889 0.38105436601704845; -0.692182777203481 -0.5430220362690558 -0.19169924364371457; -0.713848909301823 0.5682383712035098 0.21475368591818692; -0.762202012287276 0.6169631842658447 -0.06393276641993992; -0.7682887422768392 0.5658174117175422 -0.356299726756724; -0.7247484323513448 0.615681193372203 -0.3204930084782787; -0.8443101955436311 0.7531829445331782 0.35162106487694683; -0.7361591502293401 -0.7428403909252584 0.054461158094787014; -0.6989134861291908 -0.542824582709043 -0.07047657066876702; -0.7311534977516068 0.308382219231665 -0.2420265209340023; -0.7433256599203858 0.5382732546276702 -0.2395625345263195; -0.7439731882157303 0.6152077332897807 -0.2615422771160056; -0.7183921784988241 0.683166135255115 -0.25632068075573156; -0.6372607269354764 0.7800738376092019 -0.09467864945511045; -0.9264981728556586 0.8626484815884095 0.7406409970321504; -0.6596702419789453 -0.8411615509502441 0.18958949263763294; -0.20841320586198334 -0.7908230728915269 0.12046929919930525; 0.26398550226277 -0.7164725093202939 0.085019685455708; 0.4864448421040628 -0.5765963344719907 0.052561242827218184; 0.6036699781228905 -0.23314430271586686 0.02081945694704924] %
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Mass Used: 1364.498204540083 kg
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Launch C3: 97.51396636037275 km²/s²
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||V∞_in||: 10.82132158901307 km/s
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