Files
thesis/archive/ES_0.6062890058102056
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.6062890058102056---------------------------
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: 2024-05-07T19:31:29.922
Launch V∞: [6.969049236822743, -7.3945455935107836, -1.511127039897749] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.001020041596570256, -0.0015200343529773166, -0.0005737346626213739] km/s
V∞_out: [-0.0008148340880010631, 0.0015283115594991786, -0.0008248944662913007] km/s
time of flight: 1.199058110505233e8 seconds
arrival date: 2028-02-24T14:41:40.922
thrust profile: [0.3558867970377261 -0.1645591266515927 -0.19232336664940447; 0.12795322908691917 -0.0017609793282506044 -0.15892781152025712; 0.15083257816597925 0.024910932519099552 -0.2789724431057115; 0.10719561470588145 0.028448280608534993 -0.26804869596796144; 0.05543529802056861 0.017783423341576076 -0.1868669813085231; 0.044224092431353584 0.018191762097930504 -0.16477016641353126; 0.016257221500380187 0.006110492804491137 -0.06849724146923629; 0.012369442341164672 0.004998745309192237 -0.05626111288457356; 0.016158582687222554 0.006979561627480917 -0.07726721510936424; 0.010571912786472704 0.004414062452437501 -0.05547290186857737; 0.000620489809715422 0.0013157361608980996 -0.0005116649229346628; 0.0003767749990329542 0.00045305290208128165 -0.006790251538811279; 0.0009202277070379231 0.00015453547084687527 -0.0026159726594100472; 0.002022998175234436 0.002525836974137126 -0.00849427171861107; 0.0009314420495671569 -0.002600040995947044 -7.858361445901071e-5; 0.0006682962103027471 -0.0002526929527523164 -0.0008134735741905843; -0.001763767500940809 0.0028220864007451937 -0.001115219061179726; 0.00044219395649115767 0.0003797118515325729 -0.003130242327023556; 0.002010093285016865 0.0013202116661618385 -0.0016386624954070812; -0.0014463313879182229 -0.0018389288497138614 -0.0068037040745696515] %
Mass Used: 91.74284251744257 kg
Launch C3: 105.53045673047953 km²/s²
||V∞_in||: 0.0019183745088115689 km/s