Files
thesis/archive/ES_0.5575907249752716
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5575907249752716---------------------------
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: 2024-05-15T01:31:12.797
Launch V∞: [8.070300718170854, -5.669439747460093, 0.10835470047094313] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.2406200222699859e-6, -1.584508935683764e-6, -1.7761677369263673e-7] km/s
V∞_out: [1.478724083136872e-7, -7.3014841152157e-7, -1.8778145522864114e-6] km/s
time of flight: 1.8749577787493762e8 seconds
arrival date: 2030-04-24T03:40:49.797
thrust profile: [0.30256904736773166 -0.008868938423534556 -0.0993497799151667; 0.033997763500605876 0.017653108359588672 -0.04350785956165616; 0.06078991968055965 0.05017226874066922 -0.1326606240819778; 0.03210122519686858 0.03411942037764887 -0.10423299203294442; 0.034661256368489685 0.04333956680005156 -0.1489918641626913; 0.011300414204607276 0.015818592005051403 -0.06338353715588053; 0.0064478737062164644 0.008703997052747789 -0.039658530083626235; 0.008766973424181795 0.015041220948025394 -0.07025266203874529; 0.005454830247771648 0.010371987148424456 -0.05080889330162655; 0.0007415214172512507 0.0044061845132678185 -0.018717881867680763; 0.0008418447698900471 0.004407715403203068 -0.024845966405732122; -0.00036873854579050835 -0.001283685733349566 -0.0007697875436888197; -0.0021087336480423687 0.0007075677316539717 0.0008892416352340509; -9.323058119425833e-5 0.0006391604164504345 -0.00019401950028938644; -0.0017972286702230829 0.0011723418235252267 0.0033415280095845383; -0.00019982234111707358 -0.002608626632506299 -0.0030451661925102644; 4.7745546528227904e-5 0.000983965301456584 0.0006592850146664101; 0.0003697849403054275 -0.001053430877255186 0.0004672126774164019; 0.004497099695039113 0.0043447207228328455 0.004436569237040113; 0.0012309932464212715 0.0050792595711001125 0.007251086632175839] %
Mass Used: 83.03227054587978 kg
Launch C3: 97.28404147290351 km²/s²
||V∞_in||: 2.0202362053027004e-6 km/s