Files
thesis/archive/ES_0.5606392728542628
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5606392728542628---------------------------
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: 2024-05-18T05:56:01.940
Launch V∞: [7.883870910088355, -6.1046655479483025, 0.08916243925459687] km/s
Phase 1:
Planet: Saturn
V∞_in: [-8.330834933636189e-6, -6.353837337389955e-5, 0.001173598147892607] km/s
V∞_out: [4.8616753226518196e-5, -0.0011748016322134284, 2.2630886725562807e-5] km/s
time of flight: 1.8419109695959112e8 seconds
arrival date: 2030-03-20T02:07:37.940
thrust profile: [0.21008542797465665 -0.014398694030474475 -0.07909858149259764; 0.04165081266505539 0.01644035679823626 -0.06029479977616454; 0.038324300784625454 0.02564549243933937 -0.09788800263118551; 0.031288942031311565 0.022252514240205322 -0.10960368978726837; 0.030620158924168063 0.02914547997559333 -0.14291986031030182; 0.01732561982002231 0.015242187588862295 -0.0934228502390341; 0.014584247236507834 0.016182550085494084 -0.10645462653620051; 0.006650704860329358 0.006584443651425916 -0.04874863629896994; 0.003177547319827286 0.0026910172706963455 -0.024171080942469173; 0.003191040430887668 0.002887345297039186 -0.029065839536899073; 0.0007100312217510295 0.0010340096744614299 -0.009972084017789127; 0.001148133239444164 0.001466292032939342 -0.012181873699171002; 0.00023619306791280601 1.1047655437770117e-5 -0.0008591942301751053; 3.70410240713754e-5 0.00013109851388721518 -0.0006901031369148114; -1.7958902692845504e-5 0.000509524243909815 -0.0006981968617880034; -2.7475093770048045e-5 8.865460923649727e-5 -0.0005042092417528747; 0.0004733545327795859 -0.0005455859400339267 -0.0008712888765763439; -0.00026355334566069064 0.00032137565990058366 -0.0010274478307226165; 4.5361672288025e-5 -4.613015080857115e-5 -6.224935817891611e-5; -0.00014094039277459235 -0.00020086963115112974 0.0002529291442898102] %
Mass Used: 74.06899879770071 kg
Launch C3: 99.43031191981815 km²/s²
||V∞_in||: 0.0011753463916814694 km/s