Files
thesis/archive/ES_0.556531582995979
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.556531582995979---------------------------
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: 2024-05-13T05:21:40.940
Launch V∞: [8.03395379250204, -5.625721930921176, -0.1406279425842048] km/s
Phase 1:
Planet: Saturn
V∞_in: [-8.142213479652676e-6, 0.00019359714693956975, 3.414968918650208e-6] km/s
V∞_out: [0.00018793368788181346, -2.8522683154150063e-5, 4.1514873507424774e-5] km/s
time of flight: 1.8749577787837255e8 seconds
arrival date: 2030-04-22T07:31:17.940
thrust profile: [0.34448032567503517 0.0055486098265934486 -0.10668036476725423; 0.08090504029787349 0.052731692558594966 -0.089250957821484; 0.0312458473489649 0.03266100604022304 -0.06456005502321865; 0.04592215797932021 0.06723063636111902 -0.14301279320373358; 0.02221849091902015 0.040162724271196375 -0.09639132187927564; 0.02734130311054363 0.0582401754159723 -0.13814708981297838; 0.011108099585297574 0.032549935604251054 -0.08860160121962099; 0.0061756112395086405 0.0196482169489059 -0.05810759344361841; 0.0008939357267174772 0.0034097301428762275 -0.010483596075923762; 0.0007883376985772833 0.002032144086646871 -0.007426300914164813; 0.00023819751857506564 0.0006380256781959644 -0.0017978487650684239; 0.00012202123058696108 0.0002182213531806477 -0.001552020710120906; -1.555892902791066e-5 2.213912295320915e-5 -0.0001440960424583899; -0.0005648801955748456 -4.666496201067942e-5 -0.00030040144772363177; 0.0005515745622139161 0.0006774359339200597 1.4013592638286914e-5; 6.378413721510855e-5 -8.441556143670026e-5 -2.5224334190725658e-5; 7.03328670414421e-5 0.00025167766302756965 -0.0007442741671696388; -0.0002784360869930505 0.0009233792883597506 0.0010530707339470066; -0.0009202264057296134 0.0002010972350258497 0.00031533215539107754; 0.00026953557722118567 0.0005537891109768289 0.00013122089195521895] %
Mass Used: 88.04471431498723 kg
Launch C3: 96.21293700234085 km²/s²
||V∞_in||: 0.0001937983822331986 km/s