23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.646862937498053---------------------------
|
|
|
|
Spacecraft: mySat
|
|
dry_mass: 200.0 kg
|
|
specific impulse: 3200.0 kg/s
|
|
max_thrust: 0.00025 kN
|
|
num_thrusters: 1
|
|
duty_cycle: 1.0
|
|
Launch Mass: 3500.0 kg
|
|
Launch Date: 2024-05-08T13:19:38.088
|
|
Launch V∞: [7.0986916186762805, -7.509416113125887, -2.4062905368880183] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [3.768824929532588e-6, -3.5488343668664352e-6, 1.9787884999206212e-7] km/s
|
|
V∞_out: [3.907522054933168e-6, -2.587888154447536e-6, -2.1893606334908767e-6] km/s
|
|
time of flight: 1.0978829168345827e8 seconds
|
|
arrival date: 2027-10-31T06:04:29.088
|
|
thrust profile: [0.4124050712199185 -0.20704484865763717 -0.2433761072815041; 0.18454702136680454 -0.009459312277523097 -0.20636622778335775; 0.12946252094646418 0.01753061036119081 -0.21582917360043266; 0.0857976030153707 0.02053084095295749 -0.18322924484506645; 0.04530863672454939 0.013324209809296723 -0.1091049515061577; 0.01831608581364142 0.0038666251914607204 -0.04502530613103118; 0.015524633858003222 -0.0034648256610455043 -0.032678524295677434; -0.0012714918570216412 0.013723383735232632 -0.027212198033399228; -0.0035059308169837315 -0.015580796490384208 -0.04703151026846384; -0.030788589533276758 -0.016015590604932687 -0.009787675799499058; 0.04278108614038056 0.00017123630036632346 -0.03341159208453753; -0.0005185374640149015 0.009955983082417567 -0.00026780186892798145; -0.03908863695529184 -0.03162383133069095 -0.02050401097939559; 0.001397850994906349 0.009866742546415022 -0.017662281131552885; 0.10183195800504675 -0.09531818385235004 -0.10513892533387736; 0.006207930404633662 -0.015488498941657033 -0.015795870138954254; 0.06507158933289374 0.10809129921875922 0.0531604636379496; -0.014297176150757885 -0.021999391226829756 0.080992278054126; -0.02680903780431632 0.015993348870961894 -0.0018110192610280521; -0.028020466117756777 0.006564252022509825 0.07170830691312367] %
|
|
|
|
Mass Used: 97.9976683848995 kg
|
|
Launch C3: 112.57298720505639 km²/s²
|
|
||V∞_in||: 5.180484798953934e-6 km/s
|