Files
thesis/archive/ES_0.561595651578885
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.561595651578885---------------------------
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: 2024-05-14T21:10:33.498
Launch V∞: [8.168941223832476, -5.628946642745985, 0.15003508333220264] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.329080385509782e-6, -1.939730403223405e-6, -1.9470013068662964e-7] km/s
V∞_out: [1.5852690157994259e-7, -7.851957897259244e-7, -2.2193936070028194e-6] km/s
time of flight: 1.874957778749387e8 seconds
arrival date: 2030-04-23T23:20:10.498
thrust profile: [0.20697546595249544 -0.0036612754015666873 -0.07254879491337198; 0.047213649118334824 0.02346579065658286 -0.05553257024802689; 0.03253886314562879 0.02612766310531572 -0.0682941175891139; 0.03573963153517263 0.03811385878390813 -0.11288111574992878; 0.03136881199751282 0.03991897110705816 -0.13211534664533792; 0.02507373210379954 0.03631769174726763 -0.13249100307620032; 0.012722131983687573 0.020467832757757945 -0.08137030395099368; 0.005506951544842256 0.008685137561537357 -0.03781118913421742; 0.0035028649646160707 0.005572068256267199 -0.027515265641755146; -0.0024193960220556324 0.009907875976193182 -0.006640454593006529; 0.0025207584594402863 -0.0067819083955944605 -0.008564024949907222; 0.003993650884425361 0.0040368348717473995 -0.018423481785920993; -0.0007671135626293276 -0.007800033029030654 -0.004528600509874014; -0.00960471108465531 0.015670102641461372 -0.0063277839097345846; -0.003467778817540997 -6.621738961416594e-5 -0.004199663008855919; 0.0020207073240876357 -0.004914710739394307 -0.004211107231211542; 0.0011601005327634738 0.0026759418096032207 -0.006682638249067226; 0.0016282789090369505 -0.006615176854962731 -0.023416385388674393; 0.0019169302400999372 -0.00034298655441697325 0.0005635279755608364; 0.0045840161374905266 -0.01645224125865978 0.02885372861083199] %
Mass Used: 80.9665427913742 kg
Launch C3: 98.43915155154143 km²/s²
||V∞_in||: 2.3594314673720564e-6 km/s