Files
thesis/archive/ES_0.5857402350910488
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5857402350910488---------------------------
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: 2024-05-08T04:19:21.879
Launch V∞: [7.0336895840607125, -7.140316373064522, -1.1014210984522943] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.001767986668361346, -0.010255071632496515, -0.010354435857055335] km/s
V∞_out: [-0.013102076487306102, -0.0014486452108213477, 0.006522391555596863] km/s
time of flight: 1.3508728924244887e8 seconds
arrival date: 2028-08-18T16:34:10.879
thrust profile: [0.25234193560836515 -0.09923932129309335 -0.12998133461951736; 0.08730533045221095 0.0052760267147638545 -0.11008735586625441; 0.09481264323533549 0.02307730355980579 -0.1922293236264007; 0.08729509621650035 0.03018584793118997 -0.24005984716617695; 0.09231072716522187 0.03802831412759585 -0.3136332991585055; 0.05124024758562479 0.02314112041607643 -0.20636489203508868; 0.023392717142520943 0.010775653328759677 -0.10656926816150053; 0.007453881457005219 0.003906853782986809 -0.03946559666076687; 0.001752050799387213 0.0004368047231949208 -0.022012004672477752; 0.00284038392485181 -0.00045751535773871005 -0.015617067109577543; 0.0004396095552531768 9.075541417476402e-5 -0.0044374490595968765; 0.0005774577819362883 0.0004269222957302268 -0.004725012006628277; 0.0012284524192219199 0.000494217744131776 0.0007076901915737416; -0.0019309995488982486 0.0037272995548116496 -0.0014747530788319356; -0.004398356826056252 -0.0001701990321460792 -0.0004529597832389279; -0.0005568803073753747 0.003376479628554669 2.1677059920763883e-5; 0.0008757873820567439 0.0006223201347950989 -0.0003292889363419888; -0.004191146592122074 5.228833951420219e-5 0.00021148291104048972; 9.406562947620914e-5 -0.00023898407326223908 -0.0006021972612706874; 0.002400162851577539 -0.0006401898269819853 -0.003664108374455369] %
Mass Used: 90.28840047334597 kg
Launch C3: 101.6700355084933 km²/s²
||V∞_in||: 0.0146801434926574 km/s