Files
thesis/archive/ES_0.5640007460344055
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5640007460344055---------------------------
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: 2024-05-12T02:43:38.374
Launch V∞: [7.574459704813602, -6.298470455910129, -0.08207958810726437] km/s
Phase 1:
Planet: Saturn
V∞_in: [-5.804651009768497e-7, -1.185523407963461e-5, 0.00024126105492319898] km/s
V∞_out: [1.0186202125809985e-5, -0.00024132037174027742, 2.3531391274063883e-6] km/s
time of flight: 1.7006478731453398e8 seconds
arrival date: 2029-10-01T10:56:45.374
thrust profile: [0.30091487743615963 -0.043187079249355664 -0.10964636229731262; 0.08193472480447449 0.028657930755971756 -0.09526264579543231; 0.048571668790267176 0.026803582974096338 -0.09677372355723653; 0.05130061163175575 0.03885875546217573 -0.14350429734778297; 0.024651408011648463 0.02244415153983185 -0.09582924979525494; 0.03979715452053865 0.04081572039872482 -0.1760805398365952; 0.02250891208327938 0.026334508676358476 -0.12433462978660874; 0.005379106886219192 0.008563934523830847 -0.04817231021057636; 0.005736372200535223 0.008205970778898675 -0.028223215378669553; 0.005864809539225689 0.008585676403293633 -0.049489245181077404; 0.005334692165637828 0.006436390185358772 -0.043193549823483834; 0.0005373707722067869 -0.003887802653905726 -0.0031908983316144743; -0.0009419756520945687 -0.0004907700380262815 0.0003858682700847004; 0.0006485276440476735 -0.0026702498929851663 -0.0018103537129513958; 0.0001646746817005818 -4.332430389557512e-5 -0.005980495184572319; -0.0069639522601701994 0.007713434331598261 0.004097206342982618; -0.000882182958638534 -0.0003119151428563668 -0.0002684618512495589; -0.0003049789651761165 -0.003134378671878642 0.0046124449445346435; 0.003944325705418475 0.0020109370903609613 0.005004232826926042; 0.003270504475913241 0.003308780513405306 -0.004766743088474796] %
Mass Used: 91.87641309163064 kg
Launch C3: 97.04990696260157 km²/s²
||V∞_in||: 0.0002415528516442545 km/s