37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJS_2021-11-29T21:44:47.574/mission---------------------------
|
|
|
|
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: 2023-06-24T11:13:35.652
|
|
Launch V∞: [4.204198767059533, -9.994451029411268, 4.407763020256069] km/s
|
|
Phase 1:
|
|
Planet: Mars
|
|
V∞_in: [1.1816902279242838, -9.996430420980913, -3.9141617445235055] km/s
|
|
V∞_out: [0.37910175293619774, -9.534044813617678, -5.060049667159223] km/s
|
|
time of flight: 4.577040007583382e7 seconds
|
|
arrival date: 2024-12-05T05:13:35.652
|
|
thrust profile: [-0.6281059032448896 -0.9645978361567867 0.04825409754226176; -0.8740723336039602 -0.9597496199427967 0.05604914227980348; -0.897647871256038 -0.9575735835349201 0.09800966403698955; -0.8947340470580677 -0.9548346668410663 0.15634176550887674; -0.8837997723274917 -0.9506389891549062 0.2119922535014052; -0.8733870717624931 -0.9429899204491616 0.2583708134992254; -0.8720845887317354 -0.9025764262000016 0.2931913647382538; -0.8825703424810087 -0.5611857908303168 0.31198994673950864; -0.8867206383135808 0.3805834562800023 0.28726172697464486; -0.8888991630049579 0.788013986816961 0.23249659162459266; -0.8970204827538024 0.8882296727690108 0.17207243243036158; -0.9065712428541088 0.9234064642311088 0.10537365025980958; -0.9148714632891286 0.9404349357133255 0.03442544496598595; -0.9208141256954919 0.9503791830745603 -0.03567082436670164; -0.9236394768970245 0.956949522940748 -0.09754989596668419; -0.9220273833669875 0.9618350488524434 -0.1430101775953111; -0.9126940508648808 0.9660194230411197 -0.16197775579747833; -0.8857853310494002 0.9701186203520745 -0.15061297758287906; -0.8029871986880408 0.9745861477536751 -0.10435361844832336; -0.4980925964808032 0.979366793392864 -0.011905648117825195] %
|
|
Phase 2:
|
|
Planet: Jupiter
|
|
V∞_in: [-3.3293666105405575, -7.620971578491845, 1.0687733254722611] km/s
|
|
V∞_out: [-6.935603481721296, 3.497201324971365, -3.158033428514645] km/s
|
|
time of flight: 2.2417560002564985e8 seconds
|
|
arrival date: 2032-01-12T20:13:35.652
|
|
thrust profile: [-0.3656566194762257 -0.22912757683936658 0.045808165828645775; -0.5810293395224363 -0.29607251343651775 -0.13300805411577823; -0.4856402754635828 -0.4614047283645683 -0.18145385059581523; -0.2733529556486418 -0.42488777696168484 -0.1702396496601306; -0.06558140669038927 0.07510354553305262 -0.1674187982096823; -0.21526857860677945 0.45034604284055235 -0.04663600347350332; -0.4898784174638757 0.4672206097962957 -0.023748597462847795; -0.5650731143780724 0.15545877435880226 0.0018975633487120474; -0.5089407649543735 -0.33474815321731466 -0.08561486507950282; -0.41521030324056496 -0.34928781074095683 -0.1390599491503587; -0.3251150806058122 -0.22460933014070283 -0.1345228273672964; -0.21831464912318946 0.2614219842817418 -0.09124370704265022; -0.33671096662164174 0.5619362774706881 -0.03884229233090504; -0.6767648054832806 0.6334416704852173 -0.05037338528195778; -0.8062403423691754 -0.29179921474968684 -0.12036905303677174; -0.5776385810576635 -0.7669983678262886 -0.0642881827918457; -0.016220388338266608 -0.6010313543551327 -0.09290105482283402; 0.07029572715666328 -0.328415627959751 -0.11381534454303409; 0.08335842385908794 0.04906852415946227 -0.12154942027309859; 0.08187921283901471 0.3612744411676179 -0.11286850125684299] %
|
|
Phase 3:
|
|
Planet: Saturn
|
|
V∞_in: [-1.0842531035611531, 1.2406035825140813, -0.5854117544230216] km/s
|
|
V∞_out: [-0.023022631572720317, 0.023022631572720317, 0.00027223728207050724] km/s
|
|
time of flight: 4.927968000000019e8 seconds
|
|
arrival date: 2047-08-25T12:13:35.652
|
|
thrust profile: [0.35472737510521357 0.18207157177175717 -0.03254085314485865; 0.2266310259633882 0.3143675224006778 -0.01634653859009041; -0.10803902823003882 0.2896540320383328 0.03698624574214201; -0.11188790602824296 0.0915541039807244 -0.021159489070060124; -0.06936165955738366 0.05183112468149076 -0.057003976993703534; -0.04249032460536079 0.037075185269534884 -0.06367664972970241; -0.027648538697579345 0.023332194805352827 -0.05841953485870754; -0.014366139480565362 0.005827157994898504 -0.048061820566802686; -0.0022792620463178326 -0.009394651147162938 -0.03506791686081867; 0.009030269893451199 -0.02706297073989417 -0.024848503402645945; 0.019191776330403483 -0.040724325634559244 -0.013472336734798319; 0.03352802263728233 -0.0548449925970575 -0.0022387391078727108; 0.04758516117011756 -0.06820275602257245 0.010158607228174674; 0.06047608901522452 -0.08069030413927751 0.023475738159138497; 0.07126343200191616 -0.09274908219459146 0.03743668043976812; 0.0790452936746388 -0.10510006610579826 0.05145735407037108; 0.08312186020602563 -0.11864440821410976 0.06447591831670829; 0.08349578603424643 -0.1340449393883435 0.07445748197303119; 0.08231493768561268 -0.15058794815993298 0.08381258156479551; 0.08110239170439432 -0.1733639918710088 0.09588561948953665] %
|
|
|
|
Mass Used: 2029.541947000274 kg
|
|
Launch C3: 136.99271349498176 km²/s²
|
|
||V∞_in||: 1.748544813193361 km/s
|