Files
thesis/archive/ES_0.5641279507314239
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5641279507314239---------------------------
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: 2023-04-28T21:32:36.667
Launch V∞: [6.284049420067361, -7.2840600639466375, 0.23159410683089876] km/s
Phase 1:
Planet: Saturn
V∞_in: [-9.5652333005464e-9, 6.62330282536911e-10, -8.559714018367129e-9] km/s
V∞_out: [-1.8711216024954295e-9, 5.036187668545062e-9, 6.084666563247647e-9] km/s
time of flight: 1.8749577782983327e8 seconds
arrival date: 2029-04-06T23:42:13.667
thrust profile: [0.6071923945774459 -0.1348432355192808 -0.1591055820045334; 0.10518296365038605 0.03774589038707594 -0.09474707562815506; 0.06821776652494227 0.04568455552378015 -0.10432313672735169; 0.05857035376830896 0.05286694669096663 -0.12476763896045445; 0.0504171588837525 0.056844531626981165 -0.13905992202661763; 0.02135481349118263 0.02846854650803043 -0.07357532593761358; 0.015673824933689462 0.024769532243361984 -0.06881044028081335; 0.017254369834050785 0.03083206167851204 -0.09020845801775453; 0.004046481327054702 0.004892115771558467 -0.01713642258467718; 0.002782782577332919 0.004363646054162461 -0.014994284500203988; 0.005115558123359517 0.01139834625276415 -0.037230372467476874; 0.0022743568428546983 0.0024031830240484726 -0.0025428989387401846; 0.00031840328171541974 0.0003058088521384429 -0.004385216004175771; -0.0009769294458462589 0.0010810185005597258 -0.0014807847919164215; -0.002257386431266923 0.0005035094174929886 -0.0010669131683479034; -9.603694191563975e-5 -0.0012032171956549338 0.0010433926105413922; 0.0004568264282624981 0.0015644479600216655 0.00040870484533151396; -0.00015269736365839637 0.003252300235580972 -0.00021541505476068887; -8.94398495705928e-5 0.00038572484986339303 0.001693320819348974; -0.0008926874986838871 0.0022515639062345165 -0.0039001203516923627] %
Mass Used: 117.98001942378596 kg
Launch C3: 92.60044395935003 km²/s²
||V∞_in||: 1.2853056973859486e-8 km/s