30 lines
3.5 KiB
Plaintext
30 lines
3.5 KiB
Plaintext
/home/connor/projects/thesis/archive/EMS_2021-12-12T16:01:04.514/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: 2023-07-08T05:11:21.442
|
|
Launch V∞: [7.608076212455678, 2.807333338029972, -0.7296465923907695] km/s
|
|
Phase 1:
|
|
Planet: Mars
|
|
V∞_in: [8.010347423561068, 3.2469372890009143, 0.9052053694493565] km/s
|
|
V∞_out: [8.595491836222386, 0.9305961590076297, 0.8829460767922697] km/s
|
|
time of flight: 1.285682951483629e8 seconds
|
|
arrival date: 2027-08-04T06:36:16.442
|
|
thrust profile: [0.07414876190498018 0.061418074622027974 -0.012644930305191268; 0.005288427050926843 0.06622341067027271 -0.01948043031768979; -0.03963858081578733 0.046911280729787376 -0.025333966766685957; -0.0693496161126329 0.031308343596909594 -0.035395597569043105; -0.09403908126205902 0.015893237291132945 -0.047093551884514924; -0.12169201205925062 -0.0007977301725099221 -0.056349298411649505; -0.13903080782532432 -0.023716664620632603 -0.06390511581051783; -0.15450668610406254 -0.04110038684733795 -0.06471664925953435; -0.15811658018787572 -0.056770227221372115 -0.06186158450863763; -0.14688366879113826 -0.06858393095838325 -0.048462199618237715; -0.12668694389924282 -0.08632300225726315 -0.034758267139006545; -0.10530920293607691 -0.10528354810684375 -0.02720399752175047; -0.09090371755012416 -0.12194843310927922 -0.021454466137421403; -0.07844574463506924 -0.1363037266093477 -0.01574716544865601; -0.05844360196093202 -0.1515941613574019 -0.009255165942420979; -0.034312300204900524 -0.16511832855603034 -0.0009688494952381404; -0.0028992408640754097 -0.17347460518323504 0.006524027611181451; 0.03968790735981553 -0.17103970596354526 0.01802812299096526; 0.09266705743272931 -0.1535778429859241 0.025140107388620526; 0.20165971230655427 -0.14421264141271573 0.040991785807895254] %
|
|
Phase 2:
|
|
Planet: Saturn
|
|
V∞_in: [5.172452466285559, 3.681404565790302, -0.7376128757432779] km/s
|
|
V∞_out: [1.0471838805707034, -0.9458496802640074, -1.0540623554828816] km/s
|
|
time of flight: 1.3794018891807556e8 seconds
|
|
arrival date: 2031-12-17T19:19:24.442
|
|
thrust profile: [0.4631902795092741 -0.08224771535152973 -0.006480928889750821; 0.41704341820262636 0.21095659271139136 -0.02620914649646857; 0.2797622883993905 0.28592479641588525 -0.047115859690752125; 0.16999303712128083 0.27059720181308317 -0.05726221774165335; 0.10505343297735933 0.24439744913692196 -0.06242988174728664; 0.06300675973086067 0.21817544269642067 -0.06368113246047818; 0.035798514967212466 0.18835657288959481 -0.06877313709544629; 0.01319570173604884 0.17195586849080916 -0.06353926803226635; -0.0028206814647056726 0.15245841060553408 -0.06090532235092303; -0.015082533306159574 0.13455720233249788 -0.058050722168487584; -0.02467540253289453 0.11876086660610821 -0.054811640710621876; -0.03294606177558641 0.10466484376452906 -0.05156606010332461; -0.03552225607407402 0.09449768203449549 -0.04909814885511831; -0.044198382979974346 0.08219311436910662 -0.04488660247693665; -0.05192427793509353 0.07124227028180148 -0.0429911500566686; -0.06297039751477762 0.0597152997307626 -0.041771291047482936; -0.07719329504107608 0.04574422574176853 -0.04069542662253849; -0.09549593365185864 0.02256061596005478 -0.03696703906940773; -0.1044144745168432 -0.01480076697580528 -0.01798772858528922; -0.10164225283033314 -0.03637354833556879 0.00015260443811211083] %
|
|
|
|
Mass Used: 369.23128366753645 kg
|
|
Launch C3: 66.29632827513589 km²/s²
|
|
||V∞_in||: 6.391484713856986 km/s
|