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thesis/julia/test/missions/mbh_1_phase_best
2021-10-12 21:49:46 -06:00

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missions/mbh_1_phase_best---------------------------
Spacecraft: bepi
dry_mass: 2000.0 kg
specific impulse: 2800.0 kg/s
max_thrust: 0.0005 kN
num_thrusters: 2
duty_cycle: 0.9
Launch Mass: 4000.0 kg
Launch Date: 2022-03-06T01:59:18.919
Launch V∞: [-1.1356413222408823, -4.788069365262547, 2.7000635369246] km/s
Phase 1:
Planet: Jupiter
V∞_in: [0.606990343209641, 4.407893426470118, 0.9244860672598548] km/s
V∞_out: [1.2183577357736917, -3.9826645468861925, 2.3687041043301797] km/s
time of flight: 1.194581479969281e8 seconds
arrival date: 2025-12-17T16:48:25.919
thrust profile: [0.2047491180715187 -0.37019469041025893 -0.10453549807669095; 0.4301220091095493 -0.12441963747750297 -0.006770873233015344; 0.43924678986775806 0.1285374874465679 -0.07977271709638968; 0.42297198253230855 0.31380495510861767 -0.07919431310255642; 0.3614168205981836 0.39602843825488454 -0.05704653521018108; 0.2902414389460733 0.4053822027059241 -0.02821739799974643; 0.22430933743909634 0.43938508487263367 -0.00930631106824115; 0.13232647607691467 0.4188738913138919 0.007567873851875307; 0.054141732819826004 0.39551671259361465 0.010428460581952593; -0.012077434841877642 0.3792721276901153 0.0231446451624962; -0.042939891420425445 0.367704668401295 0.04590678245879779; -0.06832185713480624 0.39461571349444186 0.06647905984921844; -0.06871098668169624 0.3943544952193675 0.07996958584990013; -0.043122107121887 0.3236627227698529 0.06434542295394348; 0.0002258095938542581 0.3100245138960139 0.08315646808686966; 0.024384212213495196 0.1820219401839858 0.049878939508001104; 0.014803074731020839 0.09226807883171781 0.03031339291970727; 0.04882521682144194 0.07182823075104046 0.030435679401299; 0.07679479397181303 0.04220157719360384 0.024296177838332548; 0.07770574743624227 0.006328096858830944 0.01324607153162614] %
Mass Used: 1527.1786215537763 kg
Launch C3: 31.505632562776483 km²/s²
||V∞_in||: 4.544517160758207 km/s