Files
thesis/archive/ES_0.5580003426955271
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5580003426955271---------------------------
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: 2024-05-14T19:38:13.457
Launch V∞: [7.71805770052733, -5.742970691312375, 0.41907877012189615] km/s
Phase 1:
Planet: Saturn
V∞_in: [-4.870829305123059e-10, -8.587176798050595e-10, -1.2857878319189027e-9] km/s
V∞_out: [1.1147733718853208e-9, -9.85409121764542e-10, 5.014855532776613e-10] km/s
time of flight: 1.8749577787489814e8 seconds
arrival date: 2030-04-23T21:47:50.457
thrust profile: [0.717934323104759 -0.013471036726563473 -0.2080746970669401; 0.056626993169836055 0.03099226914678527 -0.06917864071699362; 0.023328209107715457 0.020694886015130556 -0.05244530650012631; 0.024976537138179215 0.02726236821865304 -0.07819744830058134; 0.0239395523366526 0.031800417215707755 -0.09880505014192684; 0.0222196033029608 0.03417097148434119 -0.111703623788035; 0.007881301910253307 0.01515935644106103 -0.05910527731593039; 0.011190119174775087 0.021314218314256606 -0.08073409001026867; 0.00582210892653087 0.012241903977660715 -0.04801569314828091; 0.003119289499894062 0.008425684913944884 -0.03409893496918177; 0.001364125308003873 -0.0007002562166305516 -0.0012685710174953858; -0.00013935682851654778 -0.0010258245329638675 -0.0005144231023635665; 0.00022756868827746287 0.001103453415395622 -0.007539326816034423; 3.363226110967622e-5 -0.00022541967519052884 -0.002387831756867094; 0.0004147538025109424 0.00011864327140745335 0.00020294122100734426; -0.000865639759943099 -0.00027105631770641466 0.0014407695703522795; -0.0005458560307631272 1.793624106581506e-5 -0.0011479297816184286; -0.0004847191492986777 -0.001589544943674174 -0.0029989820226423145; 0.000938312554798395 -0.0025078624331877747 -0.002320729276139891; -0.0018666198717207914 0.001181983179732636 0.0045135085294501645] %
Mass Used: 110.10016787931227 kg
Launch C3: 92.72575404550903 km²/s²
||V∞_in||: 1.6210787098463026e-9 km/s