23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.571076688355779---------------------------
|
|
|
|
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: 2023-04-25T20:37:36.368
|
|
Launch V∞: [5.673559503804839, -8.038915944612057, -0.2651614429374779] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [9.893217103557307e-5, -0.00012683314163272155, 2.171608064209921e-6] km/s
|
|
V∞_out: [3.271560368402114e-5, -7.690206710675827e-7, -0.00016490280794931558] km/s
|
|
time of flight: 1.5752961259759948e8 seconds
|
|
arrival date: 2028-04-22T02:51:08.368
|
|
thrust profile: [0.2715886080167703 -0.13111684316262331 -0.11575025232213727; 0.1393400413394519 0.004285441769110802 -0.14889351345888624; 0.08257244033433375 0.021031075137552705 -0.14297131466788648; 0.0959704449767654 0.03622279094567604 -0.22109254702888814; 0.05627506896637013 0.02705522544989773 -0.1628046593983357; 0.0796301313105025 0.042677979682752144 -0.2666764675213297; 0.019153615039933618 0.011982514197969025 -0.07785800602185917; 0.012466665205324235 0.008641488668840493 -0.05668904858066114; 0.003663684456139857 0.0023051285475642943 -0.017774680712167354; 0.0024644743291406773 0.0015942869855420246 -0.01192267630909027; 0.005638351736105067 0.0037120076912269357 -0.027605888813959572; -0.00023765659991176294 -0.00029887030600957723 -0.002549403924019489; 0.0001495754758945453 0.00017104472742313613 -0.0015840929033657408; -6.4481043638522125e-6 -0.00040499139974891425 -0.00029906924287873926; 0.00026654358723618194 -6.651285980014684e-5 -0.0014680748344123632; -0.00040567122592859904 -0.0014374897020798677 0.00022822716296675132; 0.0009835619138291154 -0.0001506435806196388 -0.0005085964563491508; -0.0024989897564533297 -0.003145165980956699 0.00020062155044801757; -0.0008102529019610092 -0.002138990065887482 0.00028581341324519793; 0.0014289023264205038 0.0018858392005319958 -0.004161843450709612] %
|
|
|
|
Mass Used: 101.10088375673377 kg
|
|
Launch C3: 96.88375759857286 km²/s²
|
|
||V∞_in||: 0.000160869313928488 km/s
|