Files
thesis/archive/ES_0.5586053441148139
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5586053441148139---------------------------
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: 2024-05-17T02:34:31.390
Launch V∞: [8.058827652448207, -5.840557898848283, 0.47212547102953606] km/s
Phase 1:
Planet: Saturn
V∞_in: [-8.960529328300668e-5, -6.55394891470949e-5, -0.004452821150242591] km/s
V∞_out: [0.00425543234892623, 0.000891970495920396, -0.0009653863185611214] km/s
time of flight: 1.8573112783415443e8 seconds
arrival date: 2030-04-05T18:33:18.390
thrust profile: [0.18594033030812315 -0.019364719116423915 -0.07416201761763497; 0.05829904357486814 0.018710959745419666 -0.08160961604563002; 0.040172408387585595 0.018823324175209464 -0.09887636718236445; 0.03840698685831581 0.020233193186512604 -0.13248445278554147; 0.02979538166705459 0.016617081941020642 -0.13105479183161356; 0.019176169477630355 0.010662930059824563 -0.09903860455674976; 0.010049587247266147 0.0056183578642874646 -0.05942720887321053; 0.003228145465330148 0.0016187736761890982 -0.02145252591299337; 0.008720793346398465 0.0050469058984568636 -0.06257490061292043; 0.0018996937051517925 0.0008047904521003844 -0.014028846800698649; 0.0004225497767852386 0.0008856330134996438 -0.006407822400711318; 0.0019987208601675486 0.000683289198007571 -0.014971417272661366; 0.0005497275138941863 0.0004453847888671647 -0.003042883290381524; 0.00012370402611770184 5.790493294844355e-5 -0.0012980801280014524; 0.00031240145574388606 -4.210893948627958e-5 -0.0010360941632663156; -8.831250507929241e-5 -2.9294346788481416e-5 -0.001648513571184649; 2.4871204796982852e-5 0.0004951529464734775 -0.0005264342602982917; -0.00018289838612690668 0.0006747493233550854 -0.0008227935007041887; -0.00013128156762720004 -0.00043757537584653613 -0.00158793538920112; 0.0009140116338973811 0.0006358691021311003 0.0009334960710307442] %
Mass Used: 72.57452218861226 kg
Launch C3: 99.27972216205782 km²/s²
||V∞_in||: 0.004454204836923168 km/s