Files
thesis/archive/ES_0.6081986584335951
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.6081986584335951---------------------------
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: 2024-04-27T13:28:24.724
Launch V∞: [7.174990566505607, -5.694087640464849, 0.8578181550236185] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.00010731512670546547, 0.0002044312798660693, 7.386928221469432e-5] km/s
V∞_out: [2.1341489092229188e-5, -0.00014095415584044037, 0.00019622390115699907] km/s
time of flight: 1.8749577775411496e8 seconds
arrival date: 2030-04-06T15:38:01.724
thrust profile: [1.0 -0.013608272016363556 -0.06960117252550028; 0.7024223120474911 0.5022965160005906 -0.19521222761637097; 0.21845030602416263 0.28735545698690423 -0.13460034643178953; 0.09620472423491433 0.17808098937912153 -0.09404826546889444; 0.034836991664896386 0.08959803257331578 -0.05327219426214073; 0.01599948110692474 0.05475355836311866 -0.03516715691182709; 0.025808155581409108 0.12227596534769072 -0.07726790004531667; 0.005942051113859677 0.03697504770508425 -0.026257978320049724; 0.00026818624930169583 0.0026552080581827365 -0.001969170348985645; -0.0006196309521831435 0.0005244217632303331 -0.00012637016858935013; -0.0004208295055710943 -0.001674078618666114 0.0004330792279821934; -0.0021178584619240904 0.0007050023638117534 -0.0006292942241252686; -0.00022515420712526245 0.001910036556055803 -0.00031668643814923895; -0.0005102111605426109 0.002567358610240745 -0.000896808862900387; -0.0002424389956418133 0.00016657016856833952 -0.00010375527781257424; 0.00026803707718483377 -0.0004099831248584704 -0.000588122470995352; -0.0013033253524049704 -0.0022463024164360813 -0.00033366915648349216; -0.0023338558135953293 0.002104799081277624 0.0015176093099419099; 0.00029240656975961334 -0.0003907985744752917 -8.000255081271727e-5; 0.004283986410085579 -0.0002511408376240179 0.001323065549584771] %
Mass Used: 215.83774340853597 kg
Launch C3: 84.63897567382713 km²/s²
||V∞_in||: 0.00024241566670164577 km/s