Files
thesis/archive/ES_0.5816020105686829
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5816020105686829---------------------------
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: 2024-05-24T22:18:11.303
Launch V∞: [7.925015702957565, -6.471348109581751, -0.6211240591766617] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.3201526018633373e-6, 1.4594374726845126e-5, -2.1191532485055057e-6] km/s
V∞_out: [2.1766998288560785e-6, -9.25245764681783e-6, -1.1363100054994491e-5] km/s
time of flight: 1.8749577771285182e8 seconds
arrival date: 2030-05-04T00:27:48.303
thrust profile: [0.13069182835879942 -0.018965410501387524 -0.06620381839916166; 0.01179242349966534 0.003942163902993892 -0.018556545346073577; 0.014775965784794256 0.001280908765137431 -0.04595328709483029; 0.0405548710055996 0.0016453392482993043 -0.16038999214695457; 0.027867596448703447 -0.0018231171503122637 -0.13561790793523681; 0.01789316007489491 -0.0028723496901642384 -0.10121221157193795; 0.012801309670833783 -0.0031242463484419157 -0.08011800222705136; 0.005679088597712575 -0.0026167584832553674 -0.03592320782024938; 0.004341989780635864 -0.0022580305917980575 -0.027975546012586637; 0.0023345998526854705 0.001273534499375564 -0.015189479105373212; 0.0016748803525490322 0.00228138943891007 -0.008394151779802489; 0.0034499610649380962 -0.0013908381882521254 -0.025129755070016663; 0.0006510013565993503 -0.0018036646439786553 -0.00397789693782426; -0.0032314956046892206 -0.00022025534562322425 -0.0016930979228215607; -0.0007587207893121621 -0.00030039605613159224 -0.0014452255307659677; -0.001955518805580353 -0.003286594569499004 -0.0008632140673434574; 0.0036108896272292143 -0.0038455411247537686 0.0031980860752099717; -0.005653363716184365 -0.00461513425411329 0.006966439847341365; -0.003573387694547449 -0.005983384582686283 -0.013061256977712626; -0.005819822639326032 -0.009494578063271617 0.0076136747015610705] %
Mass Used: 65.62725615446698 kg
Launch C3: 105.07001534439938 km²/s²
||V∞_in||: 1.4806396828750529e-5 km/s