Files
thesis/archive/ES_0.55982781382513
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.55982781382513---------------------------
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: 2024-05-13T21:55:47.959
Launch V∞: [7.828199980718763, -5.966214866018369, 0.025194065639041748] km/s
Phase 1:
Planet: Saturn
V∞_in: [2.9176577679481894e-8, -2.5810812404950547e-7, 4.824692611357479e-8] km/s
V∞_out: [-1.848913715271719e-8, 1.5573630473449234e-7, 2.1313822274573212e-7] km/s
time of flight: 1.8181198200324404e8 seconds
arrival date: 2030-02-16T05:15:29.959
thrust profile: [0.3051862882720383 -0.0036165853301262938 -0.09832178435064433; 0.046522558266602516 0.025250532607452067 -0.051367671942706424; 0.04698864449296434 0.043024659858526694 -0.09310853638670044; 0.05199703398087316 0.06600391018581211 -0.14857640627149177; 0.02993015833438498 0.044637181874884656 -0.11685924840737068; 0.017700756027484867 0.029655548126622234 -0.08648826832072742; 0.015311478648432523 0.030762376088170645 -0.09366887988181402; 0.009393307420457546 0.022531252585828276 -0.07243780859145975; 0.006778129753463886 0.016873058279086098 -0.05820584875454555; 0.0015836396986214176 0.0014099371993585843 -0.012447680654683404; 0.001003037408209222 0.0010309761208017625 -0.007202356688995392; -0.001712766138798397 0.0029688875664989475 -0.0032412292282615576; -0.0028754261820546083 0.0012085620575210587 -0.0047036307505859375; -0.00024775471630993984 -0.0005907335798309237 -0.0030553849202906718; -0.0027851874243131824 0.0030576409282282667 -0.008201109621098093; -0.00019346472465014102 0.013093988387472177 -0.0034067502894810533; -0.0005705525203458482 -0.0028114572629347225 2.2890498430122933e-5; 0.005824600076304782 0.00876716104959263 -0.0013228423104816004; 0.0009599671276473722 -0.0018490927009600987 -0.0014861764195962875; 0.0006293882532079559 0.005908939980813925 0.003062755038679129] %
Mass Used: 88.0162106743428 kg
Launch C3: 96.87706950656725 km²/s²
||V∞_in||: 2.641947052172895e-7 km/s