23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6291474847232406---------------------------
|
|
|
|
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: 2023-04-25T09:27:58.600
|
|
Launch V∞: [5.311368704105728, -8.800657967658047, -1.9990789856602607] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.1434364585395264, -0.04347854440077238, 0.09506084493934472] km/s
|
|
V∞_out: [-0.12366567763130952, -0.05208390150379153, -0.11672489524076878] km/s
|
|
time of flight: 1.1012229757002363e8 seconds
|
|
arrival date: 2026-10-20T22:59:35.600
|
|
thrust profile: [0.5869920623740854 -0.4539038110914409 -0.3507346898541814; 0.13529178654201954 -0.03217045886137604 -0.16660019889104183; 0.09320367333615483 -0.004304205106582237 -0.1663463468631132; 0.08011279119918083 0.005115164877172536 -0.18172038404433946; 0.05012939276127233 0.00683539840386369 -0.13751712771546787; 0.0509092233031922 0.00967409272213635 -0.15850457858361075; 0.030399104409315154 0.006751804061970659 -0.10809809865063581; 0.026473494180054773 0.008862104143362828 -0.10180019118344734; 0.009076318007207311 0.0036475466213676273 -0.03212918187916668; -0.0006305278384029493 0.0002260387500308111 -0.00010901404742115267; 0.003913669432643444 0.0023439974651811076 0.005114536598215056; -0.002667600498991659 0.0013466106464260664 0.005108577491519975; 0.0029319483058351313 0.002195016400525503 -0.0011842223279057234; -0.009348507112133923 -0.0026846642779726404 -0.0028934003135761828; 0.001774920917443279 -0.001279130258344403 -0.0017182948029002428; -0.007810946652462258 -0.01022837654019358 -0.025742377120837358; 0.029298421112782285 0.004908902244056016 -0.006937030040368627; 0.0036719537755199975 -0.03925428179488076 -0.004914769027613497; 0.0063331136785876084 -0.0074624687535488135 0.010107502570487328; 0.00088262014473347 0.0016470321641409934 -0.01573992792436288] %
|
|
|
|
Mass Used: 94.33061154464986 kg
|
|
Launch C3: 109.65853496556528 km²/s²
|
|
||V∞_in||: 0.17748511402974998 km/s
|