23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6834714466572724---------------------------
|
|
|
|
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: 2024-05-08T14:46:36.217
|
|
Launch V∞: [8.022060022486338, -7.469736400904679, -2.6966679944970453] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0001675211800719599, -0.002053598568068577, 0.0005525924731345358] km/s
|
|
V∞_out: [0.0006313116857898493, 0.0014448753850232034, 0.0014370079841136436] km/s
|
|
time of flight: 9.109214481577043e7 seconds
|
|
arrival date: 2027-03-28T22:09:00.217
|
|
thrust profile: [0.571760613434047 -0.2980490502005914 -0.2726611287007519; 0.32783635207430833 -0.022458581110265288 -0.25829445759844266; 0.14835874203000085 0.01891283506662272 -0.17096660125958021; 0.03449916900406163 0.008452838233560127 -0.05329352335672431; 0.009225830753682704 0.0029097692026193904 -0.017124142506184457; 0.014194891425759635 0.005099181783952624 -0.029053855125796137; 0.004865340489172339 0.0019547013100804783 -0.011081861300468373; 0.0003628959484519342 0.00022152707365017947 -0.0007247605685957194; 0.0004423533607842887 0.0003276919855285497 -0.0008405525230968031; 0.00033616419912612934 0.00023385749403464573 -0.001283236919672423; 0.0009589250910261086 -0.0001743134792772241 -0.0010394963993658143; 0.0005862285943905844 0.0004255939235704714 -0.0025173547387020434; 0.0010457572747450605 0.0006828338774530911 -0.001886728527886754; 0.0003156329083397781 0.0013814836712011964 -0.0010329797249855298; 0.00013750505927646048 8.717400623289872e-5 -0.0003912350171189474; 0.00027045600664110604 0.00011116556991674201 -0.0006579900517029059; 0.00032595188471336284 0.00030894988916536806 -0.001118606019276776; 8.204358064490851e-5 -5.846533004689089e-6 0.0013773796342068448; -0.0012367288781336403 -0.0016408682439895464 -0.00027384843946608173; 4.5792373526822115e-6 -5.253194932580197e-5 -0.0001642777558049604] %
|
|
|
|
Mass Used: 54.085862573959275 kg
|
|
Launch C3: 127.42242717591861 km²/s²
|
|
||V∞_in||: 0.002133234367319014 km/s
|