Files
thesis/julia/test/missions/mbh_3_phase_archive
2021-12-13 22:23:31 -07:00

40 lines
4.9 KiB
Plaintext

missions/mbh_3_phase_archive
---------------------------
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: 2027-02-01T18:33:11.110
Launch V∞: [-3.150497013090804, -2.3173169584138944, 0.341495631383101] km/s
Phase 1:
Planet: Mars
V∞_in: [-0.7086971873088551, -0.10655494257324054, 0.11988806590713104] km/s
V∞_out: [0.2238809651804253, -0.3118676174457644, 0.6168980985050387] km/s
time of flight: 8.953200023401788e7 seconds
arrival date: 2029-12-04T00:33:11.110
thrust profile: [-0.12186870505136849 0.09462644883825748 -0.05810534392839175; -0.030639242847821345 -0.04245910692035197 -0.0894052455624086; 0.14113718480937812 -0.11440231644835337 -0.08324956933880284; 0.2837902510213314 -0.06260096981677356 -0.0550413035881179; 0.35855908041409906 0.04073648975482989 -0.020180975564470557; 0.3729359388901653 0.15239321939968276 0.016136485697739962; 0.3362801729367708 0.23639200487749643 0.047870876871699004; 0.26251183204522277 0.2735012454673692 0.06987761022138216; 0.17815253145241594 0.2588190065709617 0.07748014522346204; 0.11663205314604401 0.2103183053176405 0.07202476138100809; 0.11053399149833462 0.17008886355865674 0.06219240053201351; 0.16138151083151792 0.16508258430710807 0.0517839189038665; 0.21005359977761767 0.21368458752750677 0.0315693543261013; 0.19623229223435448 0.2814455053854785 0.001570447612348246; 0.12163118057275962 0.3027077944605196 -0.0304471015663471; 0.050711982127557564 0.25718214500209285 -0.05394847268359673; 0.02648153137529395 0.16832831911941415 -0.05881608102540833; 0.04710479095848209 0.08697307038303437 -0.03899890258876461; 0.07958628725681302 0.06854595922468731 -0.009001942082726883; 0.08605410384534219 0.09736430380889433 0.020673442685919103] %
Phase 2:
Planet: Mars
V∞_in: [-0.86775765928764, 0.239785321439957, -0.2793440299073699] km/s
V∞_out: [-0.728269228104112, 0.22205886592425675, -0.5557724748024003] km/s
time of flight: 1.9774800534204435e7 seconds
arrival date: 2030-07-20T21:33:11.110
thrust profile: [-0.030570769176673163 0.011978049730521367 -0.1686311146776997; -0.03734362480961287 0.018449018456192904 -0.17005264964682357; -0.04542948419070008 0.025365372398860525 -0.16992835340263743; -0.05521690145245066 0.03285244672122282 -0.16774923049721527; -0.06706930468913055 0.04078685922552811 -0.16334874802709573; -0.08131104167653695 0.04884139923754264 -0.15672575498494773; -0.09819592248044624 0.05655952543787853 -0.1479650657154312; -0.11787873911002066 0.06337920264640957 -0.13717350608484466; -0.14034999306643528 0.06867765983804668 -0.12442413309677075; -0.16539190427907322 0.07179396518491549 -0.10977409185801229; -0.1925589065058879 0.07205624162537454 -0.09328712290120528; -0.22119886531630267 0.06885264399706031 -0.07507799161161761; -0.2505343015720731 0.061677462874266016 -0.05534950074382844; -0.2797189023307287 0.05017836496163492 -0.03436640779599943; -0.3079203344948388 0.03418116061894368 -0.012445205871944063; -0.334368663091996 0.013690266374333697 0.010060492482634029; -0.35838748770071316 -0.011093871325495122 0.03277754892305918; -0.37942569771654455 -0.039796379505630045 0.055325239511752944; -0.3970806444181828 -0.07189338316019264 0.07733706717380652; -0.4112725932874617 -0.10674559801233943 0.098568724917307] %
Phase 3:
Planet: Jupiter
V∞_in: [3.096628165859758, -5.54752603323759, 0.16307349334680107] km/s
V∞_out: [-0.10793078996383877, 0.0924800512858945, -0.022459388754450135] km/s
time of flight: 8.654760001509127e7 seconds
arrival date: 2033-04-17T14:33:11.110
thrust profile: [-0.5212124178884477 -0.24272925296458728 0.016173224831160182; -0.48041901371361273 -0.42824969367860183 0.03503551018937675; -0.35657251411134105 -0.5210283603639988 0.03882674235576436; -0.18159148927663898 -0.5413874907790582 0.03142458257784628; -0.021760680952925514 -0.5187437230839083 0.020044129391221313; 0.08815802808124944 -0.468755585771906 0.008811701650286144; 0.14996577274874454 -0.39950153509190717 -0.0006374540546909846; 0.1756826332108901 -0.31843613205645516 -0.007389149611688129; 0.17606438164463012 -0.23381194273364414 -0.01163475824093298; 0.159181144560096 -0.15334688886711978 -0.013041705195263514; 0.13078599845765138 -0.08380131179134265 -0.011046703931163082; 0.09565122980609836 -0.03262766659535713 -0.006008779003864255; 0.06498733257355833 -0.009875081025971531 -0.0018112250669574325; 0.057070637186324664 -0.005117739296306144 -0.0016028113399474964; 0.06624558635734848 0.0072126749803919175 -0.0040159232988713255; 0.05783875168815469 0.01498693837279799 -0.003335562522287042; 0.04729181899024323 0.02021996828138974 -0.0030204665772785907; 0.057434402651546965 0.035842653333588784 -0.00310080378363583; 0.053208582397478485 0.046380716067435886 -0.0063431045982933485; 0.02806058144310276 0.03766447626177584 -0.005388583041760812] %
Mass Used: 1879.386292887199 kg
Launch C3: 15.412208581500444 km²/s²
||V∞_in||: 6.355371275643704 km/s