23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5764390243645301---------------------------
|
|
|
|
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: 2023-04-23T21:56:17.704
|
|
Launch V∞: [5.385901444815833, -8.104883535357397, -0.22222863671079593] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [5.5735918120227645e-5, 3.4104971920223652e-6, -4.260128490767266e-6] km/s
|
|
V∞_out: [5.3960458234308454e-5, -1.3430122793223169e-5, 6.648614983784394e-6] km/s
|
|
time of flight: 1.5383794613081685e8 seconds
|
|
arrival date: 2028-03-08T10:42:03.704
|
|
thrust profile: [0.3252078549077737 -0.14417085551910458 -0.11534969978237194; 0.34388518160278403 0.03398038101471383 -0.2739102262002831; 0.11068616493639305 0.04382467466083194 -0.15511348958211144; 0.07147495207309125 0.03919730765269814 -0.13821417897234967; 0.10910262340510833 0.07159531995053381 -0.23807212187387972; 0.043952219274045495 0.03476359284527043 -0.12013859639809774; 0.05651275683559139 0.04949344458707357 -0.170261943305552; 0.01802952922834661 0.015802431948340984 -0.0657337892139076; 0.009122501773294045 0.008693587126594259 -0.03714217921892011; 0.0037117098309224997 0.005009999911842246 -0.02201818750063943; 0.001078568027476483 0.0024940607730232385 -0.0011057568935118915; 0.000633225690816785 0.003766406366831172 -0.0035283884514475962; -0.004420654349049936 -0.005604310861398192 -0.00015112278973822496; 0.00461654105541198 -0.0027272080261689937 -0.0035190252107547776; 0.0006434585991025593 -0.0033290300977992684 0.003391742837557936; -0.0019001679651606913 0.0075157479631339985 -0.0016513233627435554; 0.005195308628602662 0.002511472406208775 -0.003228992830922148; 0.004738591999201353 0.00038389754747626117 0.006476347041895103; 0.0013294920126301294 -0.005077127417512794 0.008333874488443721; -0.0013708398417529508 -0.002727938608967079 -0.002669916452845444] %
|
|
|
|
Mass Used: 119.82452889723754 kg
|
|
Launch C3: 94.74645706195102 km²/s²
|
|
||V∞_in||: 5.600243525561509e-5 km/s
|