Files
thesis/archive/ES_0.5648881303968899
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5648881303968899---------------------------
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: 2024-05-16T20:21:17.906
Launch V∞: [7.834604596371028, -6.203013523933002, -0.3300667677305718] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.5717565980371244e-6, 1.5622289547174425e-5, -0.00035919273747912647] km/s
V∞_out: [-1.0595760107205889e-5, 0.00035944139687503306, -3.849312817473002e-6] km/s
time of flight: 1.788020157462422e8 seconds
arrival date: 2030-01-15T07:34:52.906
thrust profile: [0.15924019481446583 -0.033535203341937554 -0.0633181875932863; 0.03861623668883604 0.01075770425479878 -0.05747357770914667; 0.04410420672196134 0.02334171252597748 -0.12268441016490382; 0.027507170195613148 0.01477015583035365 -0.10050033971093272; 0.021811950131368347 0.012217851898488251 -0.10100876701653504; 0.01852797908891351 0.010577880084446323 -0.10208385557181023; 0.01691076674782755 0.016736048674467346 -0.14695295326104385; 0.006924880763617789 0.0036159760831060623 -0.0505831555416587; 0.005397123842058027 0.0074077103760140225 -0.02959327769628959; 0.0072544305731350595 0.004975094708254213 -0.04605237625953275; 0.002730577921994859 0.0019189280218663987 -0.027443508320687263; 0.0006240613774366599 -0.002546394279131418 -0.005959862699697086; -0.0006924854377085617 -0.0028944545104403734 -0.006047832006077919; -0.0013056875471417716 0.003442770421759702 0.0002861077849905429; -0.0010696103486098787 -0.004279132465452813 -0.0018536438432791382; 0.004072064545464457 -0.0005948571106072125 -0.005813833366862187; 0.008068013961090397 0.009545878087831085 -0.0011089012879334998; -0.0015184811726099519 0.005052741237769861 -0.009959210890799748; -0.0017402139371313413 0.0002928456863975126 -0.009771710447094394; -0.0005222981917114476 -0.0037653137104652658 -0.00597128410354153] %
Mass Used: 75.89327695042402 kg
Launch C3: 99.96735003073387 km²/s²
||V∞_in||: 0.0003595357409316185 km/s