23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5670852650645426---------------------------
|
|
|
|
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: 2023-04-30T23:54:14.552
|
|
Launch V∞: [6.55794175039751, -7.367393210940256, 0.19555061779473137] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-6.862718983532724e-9, -7.079182309839274e-12, -7.308904397627785e-9] km/s
|
|
V∞_out: [-2.633108793039871e-9, 5.806447479993981e-9, 7.423386353646291e-9] km/s
|
|
time of flight: 1.8749577787501833e8 seconds
|
|
arrival date: 2029-04-09T02:03:51.552
|
|
thrust profile: [0.25820389484758005 -0.05638084218404618 -0.08484776317192257; 0.06098028860953643 0.02085969899423013 -0.06508232237957323; 0.05982221364106486 0.038300618083732085 -0.10579096013820641; 0.04151788027343834 0.034515296779104296 -0.10007163067382151; 0.04151687640399183 0.04328441548327039 -0.12848329475988002; 0.0372885716132151 0.04473438828668905 -0.14243768476739768; 0.021945865269758575 0.02939490254940927 -0.10246104740815551; 0.006751697081070493 0.013145520586629697 -0.043078022550868074; 0.011325290281876151 0.016134677041012645 -0.06322502019183032; 0.004139982743742262 0.006104211045472368 -0.02038320036629561; 0.0006211435515187465 -0.005161736938870063 -0.008564375465092935; 0.0009849898647132512 0.0019068856514154893 -0.008397287077221482; -0.001296680879809266 -0.0007096875891464019 0.0019365629132613868; 0.0012573100693695765 -0.0010639684400346801 -0.0045754783858310165; 0.015601725818157395 -0.005456385572926143 0.0010369759344975196; -0.001808191433557879 -0.000692441142252217 -0.004167760939380375; -0.004955811031442726 -0.0038194656977499917 -0.006095577942846289; 0.004282173146599977 0.004172449893252955 0.0014121505339042945; -0.01417830226136918 0.015328946476563413 -0.011639095345771995; -0.006852284369147942 -0.01649423486365803 0.014919615968353648] %
|
|
|
|
Mass Used: 93.88009308167739 kg
|
|
Launch C3: 97.32332277033524 km²/s²
|
|
||V∞_in||: 1.002581894188327e-8 km/s
|