Files
thesis/archive/ES_0.558398106278312
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.558398106278312---------------------------
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: 2024-05-13T22:45:21.819
Launch V∞: [7.867832291702536, -5.739414201899007, 0.13520973971981531] km/s
Phase 1:
Planet: Saturn
V∞_in: [-3.0672083738371463e-9, -1.8316427153635474e-9, -1.5482070407054929e-9] km/s
V∞_out: [-2.4283958175570325e-9, 2.1336000469205015e-9, -8.169795450342905e-10] km/s
time of flight: 1.874957778749036e8 seconds
arrival date: 2030-04-23T00:54:58.819
thrust profile: [0.4352658678251918 0.0112313340893274 -0.12206796156116129; 0.08583850127592281 0.05225207543019397 -0.09106958992409701; 0.06402661643906116 0.06369934542555034 -0.12292986465633844; 0.04637692823707356 0.06137872094784565 -0.1319076688422628; 0.031286547958356045 0.0504714129804852 -0.11952338277410338; 0.021753631162464766 0.042579994078801774 -0.11042847778107548; 0.010184997171635062 0.022029334020572635 -0.06307988439935017; 0.0019423120573132456 0.0055844291880086765 -0.016854940119934072; 0.0011583733697207784 0.001950139741510681 -0.008468484755711965; 0.0009000466556027515 0.0012492449698955077 -0.008945752725466442; -2.816277437581261e-5 0.002165548597659135 -0.0015694224601179587; -0.0006171971212129031 0.0008994525504890049 -0.006935888645926031; -0.0012200133495617101 0.0019251562836826348 -0.004908622191076477; -0.002504597203815908 0.009822834300464541 -0.0036768204609137385; 0.00014504041042958296 0.0016807287540962575 -0.00600610929257033; -0.00027427860342540316 -3.9457730327996984e-5 -0.001963838875564928; 0.0007847257468077826 -0.0004821972128173738 -0.0009897361097001975; 0.012477888693083514 0.014152308138101248 0.012192373514371298; -6.817924588977883e-5 7.573025963202853e-5 -0.00010580854240357018; -0.004464838030546048 0.0010058396574011402 0.003544779809220409] %
Mass Used: 98.10312884534233 kg
Launch C3: 94.86194202503229 km²/s²
||V∞_in||: 3.893536603933642e-9 km/s