Files
thesis/archive/ES_0.5593301011419318
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5593301011419318---------------------------
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: 2024-05-14T12:42:38.007
Launch V∞: [8.117634710382866, -5.639337045017684, 0.11027598665670847] km/s
Phase 1:
Planet: Saturn
V∞_in: [5.381356330368787e-6, 4.090073528713957e-6, -5.27497349519701e-6] km/s
V∞_out: [1.2451234729770698e-6, 8.474920581341555e-6, -3.9153015953184734e-7] km/s
time of flight: 1.8749577787451932e8 seconds
arrival date: 2030-04-23T14:52:15.007
thrust profile: [0.2575510850519437 -0.0007190397671687425 -0.08122053817194408; 0.05435490118265936 0.030912738248122962 -0.06447207773446478; 0.04325307484057347 0.04218256752134908 -0.10223105751996645; 0.02686349783287257 0.030533847612051145 -0.0792752724624314; 0.02308248969686625 0.040665234413946545 -0.1170931598254555; 0.01118522552287161 0.018487771813702224 -0.05933012001127929; 0.01380186388138076 0.02661901748567766 -0.09010112201695841; 0.01016668716758236 0.021763447315993233 -0.08043965693848158; 0.0019774501306946118 0.0042796849762567445 -0.018991149523322395; 0.0013327285138281307 0.009679681444560342 -0.03376119061442025; 0.004386038974706471 0.010768845191158182 -0.050220074637820855; -0.0008330114480277037 0.0025483352635092046 -0.003988157233443887; 0.002870641165663097 -0.0007647708498633827 -0.006907417057460568; 0.0027461963166482044 0.005821371999172647 -0.004011973300767947; -0.003656993429920376 -0.0012078991908318843 -0.0005954152935094791; -0.0009935850946042994 -0.0005471211216627127 -0.006374689103662923; -0.0035798964808609534 -0.0024467098164428205 0.004355578118616182; 0.002072946947897084 -0.0026763429900887445 -0.006823672501231694; -0.0011011991455013581 0.0026189261421026254 -0.012741274713993743; -0.0016675598320418656 0.005117821037962551 -0.004179923865362607] %
Mass Used: 82.57517238035189 kg
Launch C3: 97.7102763917546 km²/s²
||V∞_in||: 8.573974737525053e-6 km/s