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thesis/archive/ES_0.6317424223240633
2022-04-18 10:59:25 -06:00

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archive/ES_0.6317424223240633---------------------------
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: 2023-04-22T10:29:21.348
Launch V∞: [5.135807736867101, -8.500475570450726, -1.6078292527467992] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.7806246312036199, 0.21748331395429965, -0.5372179094735652] km/s
V∞_out: [0.7079830042289732, 0.2769224603449566, 0.6230148360815422] km/s
time of flight: 1.1101166893228304e8 seconds
arrival date: 2026-10-28T07:03:49.348
thrust profile: [0.9845206088722515 -0.7724072165895721 -0.5496260529491717; 0.4374653116426381 -0.10227256308762384 -0.4303523746302623; 0.2854995090497823 -0.008391488718308762 -0.4010455436964456; 0.062207790763619424 0.005086553428116228 -0.10641979957951857; 0.02380056398158796 0.0036731005314260537 -0.04589087678977107; 0.01718859033196287 0.0033744537583986077 -0.037995487165822774; -0.0017728678729449 0.003104061351784532 -0.012844730992839108; 0.03347094955205633 0.008827767271274156 -0.09149434728866915; 0.02393233728545871 0.007151023669366723 -0.0594693154269624; 0.009303962190206568 0.010575528425227064 -0.0458035143263619; -8.69853890903547e-5 -0.00013550184270143023 -0.0013372775417645924; 0.010433734845349207 0.004969696933949109 -0.020376085950333602; -0.026554617810339826 0.019121736371532246 -0.048423886563496985; 0.03320934527477721 0.020949101734041457 -0.0038987296745958; -0.0011382042335788744 -0.0002181102631965374 -0.002524840448941452; 0.0005844480382808353 0.04136918641441972 -0.07292648987571036; -0.039532274480080856 0.02908909189589312 -0.04961034790236156; 0.025210819258729388 0.047245349782968134 -0.00392688263616893; -0.034631687618247205 -0.03789625989486359 -0.015567285095111651; -0.0012433735659417677 0.007049436228626401 -0.0031955206845195087] %
Mass Used: 146.5844538954293 kg
Launch C3: 101.21972093988191 km²/s²
||V∞_in||: 0.9722535106388044 km/s