23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5597152208325529---------------------------
|
|
|
|
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: 2024-05-11T22:10:54.781
|
|
Launch V∞: [7.945999115410295, -5.542630446300323, 0.12770164781342994] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.2883543971906036e-5, -1.088470624384102e-5, 8.267446807108453e-6] km/s
|
|
V∞_out: [-3.0878296724755518e-6, -1.8415452581269278e-5, 1.017247826457355e-6] km/s
|
|
time of flight: 1.874957778745955e8 seconds
|
|
arrival date: 2030-04-21T00:20:31.781
|
|
thrust profile: [0.5496632639006216 0.0111548586653341 -0.14489488962155503; 0.10243017393312458 0.06473289110256832 -0.10886551161184213; 0.03669308957976266 0.03716931076498816 -0.07522317148555271; 0.0366644176853556 0.05186954343974663 -0.11276503114281496; 0.02624966770615412 0.04712204703246439 -0.11206195495695011; 0.014604157863937749 0.031785174511726 -0.0826022723250011; 0.008562787427870963 0.022511553895681012 -0.06381350508390209; 0.005116743454784507 0.012738298729852505 -0.03892614420255071; 0.005698774413598972 0.018566015214451982 -0.056083945873059496; 0.001418073674498062 0.0055813606233803045 -0.018461384219598455; 0.0009836447945487598 0.0038761008556366045 -0.01465620296754074; 0.00043078013165041157 -0.0011268157077181239 0.0023876806311918263; 0.0012558803991594525 -0.0016410787130475154 -0.0005051097873702202; 0.0009668600776744982 0.0018825900770520953 -0.0029163385451863887; -0.00314032482169264 -0.0006023670203746045 0.0025364499487385474; -0.00034303242482904776 0.0006468636687052971 -0.001963309078001997; -0.00035136072386121185 -0.0053699621815128645 -0.006991110649690415; -1.3833679604628366e-5 0.00320203207412933 -0.006170702584976412; -0.003657472951053046 0.004418313839464753 -0.002526987811123577; -0.00056264570033593 -0.004890938099298454 0.0014375336845740654] %
|
|
|
|
Mass Used: 105.39131312091558 kg
|
|
Launch C3: 93.87596191721077 km²/s²
|
|
||V∞_in||: 1.8783322709231075e-5 km/s
|