Files
thesis/archive/ES_0.5566941660750362
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5566941660750362---------------------------
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: 2024-05-13T01:58:02.568
Launch V∞: [7.951677713203706, -5.566022981042178, 0.23762683285748656] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.444200979710117e-6, -6.023476210815145e-6, 1.0713133204314155e-6] km/s
V∞_out: [-9.581349601794992e-7, 3.6506005978057216e-6, 5.027359572293955e-6] km/s
time of flight: 1.8749577787493068e8 seconds
arrival date: 2030-04-22T04:07:39.568
thrust profile: [0.5562611282967207 -0.006559039607227894 -0.161611149613492; 0.0525516210917335 0.029655381335413837 -0.0633553330688502; 0.05394641596828316 0.048860522534795885 -0.11272289845511806; 0.023182940291047116 0.02694862547041718 -0.07378599697929664; 0.02405510549258132 0.03626062751813803 -0.1024555099659654; 0.01477082781472045 0.02570730634009932 -0.0821534261511778; 0.007957072509201165 0.015346306620610317 -0.0543626276548184; 0.01510598110037829 0.030481662403695334 -0.11065884133689584; 0.005968687358478782 0.013983286420603949 -0.05747782037176957; -0.001086438639253237 8.575046824168002e-6 -0.0028840515933220637; -0.0007985781387333168 -0.000902595082652334 -0.0016085169671143187; -0.0005729824038799185 0.0018761054839033255 -0.0030240733739625323; 5.20085015653938e-5 0.0004654538785918478 -0.0017153994233838896; 0.0004552536338477851 -0.00072180235735298 -0.00013118975193806702; 0.0006782365611166872 0.0008921842632961006 1.4677013481626292e-5; 0.0009239347633101203 -0.000516138242245014 0.0012743989165617572; -0.0004570365917504146 0.0012618910978514687 -0.0011624223571139972; 3.075406552338305e-5 0.00017354198231468298 -0.0008216536985661195; -2.3663325951841778e-5 -0.00018196240215658655 -0.0020823786600055482; -0.00033778877809103615 0.001203894532005604 -0.00040019989844066145] %
Mass Used: 99.59002913511858 kg
Launch C3: 94.26625679184406 km²/s²
||V∞_in||: 6.286150997437575e-6 km/s