37 lines
4.9 KiB
Plaintext
37 lines
4.9 KiB
Plaintext
/home/connor/projects/thesis/archive/EMJN_2021-11-29T17:22:43.432/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: 2024-12-23T15:19:18.306
|
|
Launch V∞: [3.7246340359905252, -0.7668922286241167, -1.2982795287623152] km/s
|
|
Phase 1:
|
|
Planet: Mars
|
|
V∞_in: [2.494283608647667, 0.4779176399654301, -2.4127945752092663] km/s
|
|
V∞_out: [-0.4965998694292626, 2.280726103742723, -2.6122161933665495] km/s
|
|
time of flight: 1.1112593378745796e8 seconds
|
|
arrival date: 2028-07-01T19:38:11.306
|
|
thrust profile: [0.574314864465574 0.4270452174232693 0.29638159374668793; 0.5446571483586893 0.6545005999072503 0.29885454938460493; -0.6407008818388138 0.6047471705598826 -0.3611107482397214; -0.6090910018886806 0.4086292020353647 -0.3182239029023878; -0.5972700374128047 -0.5925649766181501 -0.1428611882223418; 0.7035933873557789 -0.7374496458897967 0.25856313264181247; 0.6187581048385012 0.71068635783626 -0.05789366680034934; -0.6641950503565809 0.6437898522192934 -0.27526162728737996; -0.7420417902057971 -0.41426865914506017 -0.23642243903474278; -0.6117186284649462 -0.7691378662390483 -0.008551868685930122; 0.9103799821363571 -0.6958464571429571 0.20143430274286617; 0.6949604843307996 0.7921653784196445 -0.06766318190720352; -0.711280843553026 0.7699727320198064 -0.2712015558254371; -0.8157341118174929 0.47411989191797727 -0.25649460581099315; -0.8017585640901678 -0.7742154973052455 -0.037675698291696834; 0.04044429011740304 -0.8663007134481628 0.2032563083072973; 0.854373492928133 -0.7735870663242215 0.19757822091240435; 0.8364988214950911 0.8495507135624523 -0.07245450181745107; -0.17309103497250355 0.8763214931380413 -0.2655879782455708; -0.8411527513899564 0.819160378514693 -0.2586467736093903] %
|
|
Phase 2:
|
|
Planet: Jupiter
|
|
V∞_in: [-5.538205957708029, -2.9054361894143304, 0.33552637947187924] km/s
|
|
V∞_out: [0.5046777525076017, 6.240066179835522, -0.1810924190839511] km/s
|
|
time of flight: 1.5845886601650202e8 seconds
|
|
arrival date: 2033-07-09T19:59:17.306
|
|
thrust profile: [-0.9036543510864951 0.6541143791625612 -0.3222980415291042; -0.8832461130197783 -0.737424683011361 -0.3022522605581414; -0.8209657934438149 -0.855511836631351 -0.2551798333859342; -0.6867673786369394 -0.8683395906979817 -0.2263222463630974; -0.4869220845452508 -0.8445214158833173 -0.20970174656218277; -0.20841896070390353 -0.7994903923698052 -0.20870160122576703; -0.013585575385545936 -0.7383743288456648 -0.1919873808978343; 0.04620627341952782 -0.6700807074028765 -0.1848557385194478; 0.049421838780437675 -0.590097708762824 -0.1747481413522336; 0.012575602179280861 -0.895741483645297 -0.1611163452378958; -0.01613975443303747 -0.4787302006004795 -0.15227094975068786; -0.06374834913614788 -0.41745586732624557 -0.13522213977947276; -0.11463100448525404 -0.36122938863930504 -0.11744005758165722; -0.1621639112103503 -0.31724876310417627 -0.0958874392701142; -0.19648220854838322 -0.264314663849154 -0.066076328071633; -0.24485223518636903 -0.1836441254903296 -0.04896203316737631; -0.2546968905066618 -0.16905466281492817 -0.022816834037144577; -0.26867493243738294 -0.11533995019061173 0.003308757184394887; -0.32378451108160405 -0.03869230342562393 0.030203817435557827; -0.32950610082115867 0.026204868836291285 0.059545893198771155] %
|
|
Phase 3:
|
|
Planet: Neptune
|
|
V∞_in: [9.265725092936133, -9.786832491497965, -0.08265318279988049] km/s
|
|
V∞_out: [-0.04939156370003244, 7.080398077984083, 0.008343683362610646] km/s
|
|
time of flight: 1.1790191001194214e7 seconds
|
|
arrival date: 2033-11-23T07:02:28.306
|
|
thrust profile: [-0.03898824639829615 0.16371784077873527 -0.00013552715761737044; -0.03965980066394493 0.16534224208941117 -0.00011383530680316276; -0.0408187339699479 0.16443725546158428 -9.400453754275044e-5; -0.041109678864468216 0.1647205038566749 -8.342084332467601e-5; -0.04174133700362553 0.16664340240392897 -7.006086027666118e-5; -0.0424810737661852 0.1667002978899254 -5.700029092451851e-5; -0.04239207210941273 0.16701251418502575 -4.383623068936747e-5; -0.04652037459029391 0.16804035967999092 -2.978584844002596e-5; -0.04427137548076659 0.16950248273838245 -1.5426422905404063e-5; -0.04508723711412531 0.16561986502047163 -1.3433623473967066e-6; -0.04558502556546034 0.17116968335570643 4.062370321680114e-5; -0.046116752045498706 0.1722075533700207 2.3987312014333166e-5; -0.04709823531387585 0.1715653407790682 3.545164619148473e-5; -0.047773360118737326 0.17247757474396616 5.171911800828078e-5; -0.04877410118731465 0.17444398529369937 6.339628403937785e-5; -0.049033599874160665 0.1739487314179798 7.666428673687004e-5; -0.050091444345239274 0.17443171851273329 8.994289395414832e-5; -0.05049095135560994 0.17620949694675078 0.00010428768262633634; -0.051247933732248764 0.1760232752199048 0.00011912360582272222; -0.052158341276396 0.17808218005608098 0.0001313980216301485] %
|
|
|
|
Mass Used: 1726.4616690486366 kg
|
|
Launch C3: 16.146552127186432 km²/s²
|
|
||V∞_in||: 13.477484307656734 km/s
|