23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.562213320034954---------------------------
|
|
|
|
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: 2023-05-03T07:47:21.915
|
|
Launch V∞: [6.643676600452952, -7.45704474939463, 0.07175917488542985] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-4.148544692455484e-8, 7.9548097110352e-8, 4.521263847149818e-8] km/s
|
|
V∞_out: [-2.8440931898729493e-8, 5.3987917663610004e-8, -8.000036059129506e-8] km/s
|
|
time of flight: 1.8749577787493798e8 seconds
|
|
arrival date: 2029-04-11T09:56:58.915
|
|
thrust profile: [0.09690198715556751 -0.02677510227905619 -0.03930045348364149; 0.045119026248167354 0.009399752284342752 -0.055657243263405404; 0.04813627471517229 0.020168180277873444 -0.09928514750328497; 0.04478589722810978 0.024890991622567724 -0.12878834770886424; 0.03946576253711902 0.025785511507557448 -0.14430126346797223; 0.0269875648167983 0.019648052804191567 -0.11967930230645607; 0.022072422165637196 0.017468136210316548 -0.11425440184220732; 0.014332103100273446 0.012020843282821735 -0.08502735162985653; 0.005776559421698036 0.005169177807335604 -0.04034112869922414; -0.00027700815456282817 0.000786572518042783 -0.00405303426807914; 0.0017390239718144455 0.0017918733896451293 -0.014314890492371004; 0.0008064385858354629 0.00026663868118260314 -0.0010144397535417008; 0.0010109928777209233 0.00025605732352863614 -0.0012454348895992048; 4.985218002159862e-5 -0.0001167347139728425 0.0008649226174466682; -0.0011341636337767976 0.00028768158323780844 0.0009845442324340464; 0.0010696252003387597 -0.0003835904584437223 0.0005703204936121976; -0.0033896126386594424 -0.00023152816631347595 -0.0022019993535902314; -0.00012189078044082759 0.0010974446842501855 -0.0014483287565695358; -0.00036535435895757213 -0.001986644848269911 -0.0024195582148905334; -0.0017185589551667777 -0.004048458134395428 -0.0008187656014241437] %
|
|
|
|
Mass Used: 74.03409686126088 kg
|
|
Launch C3: 99.75110454506036 km²/s²
|
|
||V∞_in||: 1.0046454468100895e-7 km/s
|