23 lines
1.9 KiB
Plaintext
23 lines
1.9 KiB
Plaintext
archive/ES_0.7059200527022844---------------------------
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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: 2023-04-23T07:21:41.503
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Launch V∞: [5.347657014108514, -8.446040993535144, -1.9703234612230816] km/s
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Phase 1:
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Planet: Saturn
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V∞_in: [-4.7252720004262435e-6, 2.357363886922983e-6, 4.492849619282846e-6] km/s
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V∞_out: [-3.0334037544730216e-6, 4.364891243949767e-6, -4.455399853729173e-6] km/s
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time of flight: 1.2844346581015225e8 seconds
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arrival date: 2027-05-18T22:06:06.503
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thrust profile: [0.2508928310757564 -0.16839783744050868 -0.15394292827397985; 0.1497493629833447 -0.01580422528070588 -0.18896912739096253; 0.14561962587762747 0.016274964077760568 -0.26792302658001593; 0.12110506751790223 0.029438698453759835 -0.29036820025576165; 0.08008871304561573 0.02846767508437284 -0.24086883946350507; 0.02976168857862409 0.018174924137805536 -0.1380876315849644; -0.03121291827838735 -0.02004221837783908 -0.12783783013380606; 0.10866765881998955 -0.008008547195784942 -0.04574692696075756; 0.01918777265908566 0.017226075903047845 -0.0011168223919559156; 0.028466748253105897 -0.025252412758083143 -0.0582932011843876; 0.18204191856353996 0.07685526445036606 0.06433509304356733; 0.16771169935460442 -0.2335539856048301 -0.04107759954464611; -0.12562161195097787 0.1559362471442369 -0.13307877271527574; 0.07527849747483438 0.030697633050902902 0.1944693377156965; 0.026815798464955028 -0.09793039114475607 0.08840050902644644; 0.10968742742770168 -0.2025269389018637 -0.026954586406143524; 9.162520142719211e-6 0.07771948925814168 -0.02216087302257045; -0.24826164399564826 -0.05087048766519422 0.11101234609124483; -0.02376808993348636 -0.035211450697626406 0.0998533026459278; -0.04986985278800439 -0.241329633687976 0.47310059257520437] %
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Mass Used: 217.98461996261221 kg
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Launch C3: 103.81521854686622 km²/s²
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||V∞_in||: 6.933329479757245e-6 km/s
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