37 lines
5.0 KiB
Plaintext
37 lines
5.0 KiB
Plaintext
/home/connor/projects/thesis/archive/EMMJ_2021-11-07T16:11:36.123/mission---------------------------
|
|
|
|
Spacecraft: bepi
|
|
dry_mass: 2000.0 kg
|
|
specific impulse: 2800.0 kg/s
|
|
max_thrust: 0.0005 kN
|
|
num_thrusters: 2
|
|
duty_cycle: 0.9
|
|
Launch Mass: 4000.0 kg
|
|
Launch Date: 2023-10-04T23:54:18.571
|
|
Launch V∞: [-1.0946372744813206, 1.772856344640237, 0.6518921748479192] km/s
|
|
Phase 1:
|
|
Planet: Mars
|
|
V∞_in: [-2.468570935539311, 3.9145499143885183, 0.294185580247984] km/s
|
|
V∞_out: [-1.0716225311162524, 3.7979475765527537, 2.433225426462671] km/s
|
|
time of flight: 5.03315786710681e7 seconds
|
|
arrival date: 2025-05-09T12:53:56.571
|
|
thrust profile: [0.05761170096388485 0.0037768374968660183 0.021446902745431394; 0.2338910222642935 0.038442540157432946 0.07384370283448043; 0.3763154163892285 0.15798877805762376 0.10760306536830927; 0.44522680521020497 0.3325874829511538 0.12042194905157132; 0.43452219983563223 0.4761595527593114 0.112248412068997; 0.35455482283622286 0.5534063389960954 0.08620789727452381; 0.22637206987130523 0.5641403611112387 0.047320282881539735; 0.10563883830837441 0.5173755101163249 0.0020211160360646316; 0.08552855616331344 0.4304437643000631 -0.04218486298987761; 0.1960853756766005 0.3596225932161036 -0.07804050817173727; 0.36832809338191125 0.41628231583740644 -0.10121628933922924; 0.4357323056908466 0.5885680060443318 -0.08777037764641167; 0.19220878836448985 0.6988618533998787 -0.02928321108356858; -0.3260372445818445 0.6741273897794257 0.04276866734928403; -0.4765259655030003 0.5334483571862702 0.09600999744682062; -0.43336445416827124 0.32586427042694366 0.11746957265742869; -0.3020278694727908 0.14307106565129288 0.11022531383572896; -0.13802052724283995 0.0283940948753469 0.07716223945632268; 0.000379994255704275 -0.02970595003409978 0.00908639547659395; -0.008600438414250629 -0.00609678077148597 -0.0010028719112170669] %
|
|
Phase 2:
|
|
Planet: Mars
|
|
V∞_in: [-2.4967999712121305, 1.1505263293360948, 2.948442751619554] km/s
|
|
V∞_out: [-3.1906741181460436, -1.6861119385410752, 1.8063767169662492] km/s
|
|
time of flight: 1.733327609059168e8 seconds
|
|
arrival date: 2030-11-05T16:53:16.571
|
|
thrust profile: [-0.0017142861123577843 -0.007699559345150912 -0.006388535937084047; 0.017904027729335064 -0.010463864728501053 -0.012211253494710993; -0.11452589870067577 -0.22152358678387732 -0.0210809740841956; 0.01156443159091045 -0.003897368532065136 0.004479440617280323; -0.0018576450376501718 -0.0007623677091815274 0.0017808732034867247; 0.009993325332786733 0.0014150710040253416 -0.000512307205177813; 0.002647239103741267 -0.0013242606436760882 -0.004976891838670212; 0.014924541796774602 0.0037605945568966142 0.009596392756040205; -0.017618584749391118 -0.017529516289992483 0.019033520509682534; -0.026042865995432426 -0.0865312956614177 -0.011374581928173356; 0.052154252911354115 -0.13213003153993366 -0.05375112701888339; 0.0020590554705049204 0.01030638727355359 -0.0016438826565531737; -0.00014214150335625986 0.0033114821791039133 0.006549338245203575; -0.07377901396357853 -0.03027409142259342 0.03084760058305368; -0.06206451078100525 -0.3063894058582564 0.005825322685388118; 0.17699628309895177 -0.3111676416860315 -0.10663911315716215; 0.05964752199148081 -0.005831291932262422 -0.04999533519370418; -0.004431558848567231 0.007860815818719002 0.0013374590748647765; -0.15456383911087573 0.028309448158751086 0.11359293087912255; -0.39271294367560633 -0.29698573943715145 0.17818484103244142] %
|
|
Phase 3:
|
|
Planet: Jupiter
|
|
V∞_in: [1.4924422600995255, -5.560592732188845, -0.4685665727537283] km/s
|
|
V∞_out: [0.2666192989414379, -0.035476903402614585, 0.4252672489349129] km/s
|
|
time of flight: 7.801559990038186e7 seconds
|
|
arrival date: 2033-04-26T15:53:15.571
|
|
thrust profile: [-0.05667547933380966 -0.34967018073611944 0.002732189029373461; 0.010392070890743524 -0.38900231469874 0.012454157781016004; 0.09333137039669492 -0.3933837603455368 0.02000090481188271; 0.15503747405291288 -0.3683065023975787 0.025757684941636973; 0.18293674988995412 -0.3205125326753517 0.029768540395580415; 0.17930535445082396 -0.2591475229314961 0.0318370703301853; 0.15076970710143955 -0.19372274550885235 0.03170102566964771; 0.10458817867769576 -0.13175745133709596 0.028987564999421418; 0.04878214365636921 -0.07674432001861356 0.02291451019660362; -0.002030516198702912 -0.02688349362194637 0.011613325437291943; -0.006034286792027756 0.004438215059932985 0.00017918447185226728; 0.005445584386242583 -0.00816473676350179 0.004379586882810379; 0.002909662764884706 0.00012505110525283484 -0.0007139817309227709; -0.002056634454649893 0.0030597981679055665 0.004983246314934733; 0.023984266237933233 0.012127202259832088 0.014123155751866866; 0.015229836090100148 0.0882800459102248 -0.0010477895180961438; 0.02210000369026799 0.014238614166865187 0.005816636018140111; -0.0020399990692374255 0.004805026000813184 -0.0010618970952335149; -0.04612931543476969 -0.0038678412517168994 -0.01979479274534377; -0.0331200841636588 -0.02846676207386028 0.0062777303019229585] %
|
|
|
|
Mass Used: 1973.258531533688 kg
|
|
Launch C3: 4.766213789042987 km²/s²
|
|
||V∞_in||: 5.776428833293505 km/s
|