23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5628691150507658---------------------------
|
|
|
|
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: 2024-05-11T03:15:14.787
|
|
Launch V∞: [7.703589747976635, -6.211850169696722, -0.0924716527681368] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0006468181645442435, 0.0004322729468982248, -0.00026950656916856084] km/s
|
|
V∞_out: [-0.0003543917915573563, -0.0006090307763685359, 0.00042577895375054157] km/s
|
|
time of flight: 1.7017844266181627e8 seconds
|
|
arrival date: 2029-10-01T19:02:36.787
|
|
thrust profile: [0.18572781871512076 -0.025360060517731316 -0.0702891723552638; 0.09138997361020969 0.03425255294241374 -0.10686852501732161; 0.0702538816502784 0.04481560778181779 -0.14156881411346572; 0.052143893716193206 0.04300710762334568 -0.14988864582008848; 0.0421096157810119 0.04097712042847211 -0.15754386980853105; 0.024939913747511526 0.02719430446686366 -0.11664011100271482; 0.009731362557325696 0.011728335730391982 -0.05425058899385777; 0.014340710811258714 0.01928192096877674 -0.08869742489985552; 0.013651034611960891 0.0193943702236139 -0.09520810735330143; 0.00042877271614857036 0.0012376562532596005 -0.0037247016138513564; 0.0007516674980766005 0.0021315253204121074 -0.008602798755808043; 0.0002143707759904786 -0.00029679786799138624 -5.051881886390685e-5; 0.0021339840181077326 -0.0002799042888515337 -0.0017052117822820316; -0.0003972022094972621 0.0005274029907452996 -0.0030740224555123653; -0.00022142911790649794 -0.0014178997502566266 0.006808997851922223; -0.000331078599533065 -0.001430354240117575 0.004159420672944848; 0.0014153524659083947 -0.002648392318034691 8.52122373939748e-5; -0.00015953644161923196 -0.0005668663666590255 0.0026468734473091143; -0.000298588238084794 -0.00633368824058338 0.0038078479513294194; 0.00011802296498588923 -0.0009517197852706775 0.0055215023940623316] %
|
|
|
|
Mass Used: 85.35855106155759 kg
|
|
Launch C3: 97.94092854245757 km²/s²
|
|
||V∞_in||: 0.0008233270488872985 km/s
|