23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5915125899325326---------------------------
|
|
|
|
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: 2023-04-29T18:29:06.935
|
|
Launch V∞: [6.485921189009788, -7.388745051476015, 0.24113312366023495] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [1.2563252479870891e-6, 0.0003948084914098055, -0.0002946331286379544] km/s
|
|
V∞_out: [-0.00023351961619618738, -0.00042773164933003385, 7.170156567777677e-5] km/s
|
|
time of flight: 1.844514108066306e8 seconds
|
|
arrival date: 2029-03-03T14:59:16.935
|
|
thrust profile: [0.30429273067808804 -0.08056822759907678 -0.09887741253316544; 0.06236630360044868 0.017291997770420363 -0.05324929800400836; 0.07024322239710698 0.03855346681432963 -0.11250914948883141; 0.04383580632142736 0.031380718374884556 -0.08940353066553494; 0.045407438538179835 0.041678201111027526 -0.1336184839125876; 0.0377996237344507 0.034626112231828245 -0.11781122221422284; 0.022036356609691967 0.026998955255950054 -0.08315739584605128; 0.0055129064724458166 0.01317812302650826 -0.029864906377753134; 0.006106867263902334 0.008013234435518195 -0.018642732497393472; -0.0018904926593582426 0.011063477122971097 -0.015344106943569646; -0.0020436378990615154 0.007900276082164034 -0.014451664695721449; 0.0022812672822184314 0.0017181829332282093 -0.016635139813986132; -0.002527602861849736 -0.005693624473139151 -0.007279230570793067; -0.04457307987591259 0.010835273192901817 -0.06968745451153646; 0.012728032823257412 0.01111279433496502 -0.03652418756178407; 0.026985087287126723 0.00841470734045494 -0.010064134508007307; 0.05231776527830545 -0.05166644174744767 -0.11597147804418648; 0.02192557274918387 0.023430820064725834 -0.0951684271351102; 0.10487890521776855 -0.026905931196884187 -0.04657005075680092; 0.03492131950867737 -0.030140014827868676 0.04789856745251152] %
|
|
|
|
Mass Used: 125.9045999016339 kg
|
|
Launch C3: 96.71887228908358 km²/s²
|
|
||V∞_in||: 0.0004926296821481676 km/s
|