23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5765866860154715---------------------------
|
|
|
|
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: 2023-05-07T05:44:16.338
|
|
Launch V∞: [6.251788204724815, -7.952459961293305, 0.12447828333556127] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.8756651617763038e-6, -1.1645376725119282e-6, 7.673259415377204e-7] km/s
|
|
V∞_out: [-8.264871580654765e-7, 1.8780556996738649e-6, -1.1164930532058143e-6] km/s
|
|
time of flight: 1.8056720048357582e8 seconds
|
|
arrival date: 2029-01-25T03:17:36.338
|
|
thrust profile: [0.08364529623247598 -0.03840692562005442 -0.04491750451280783; 0.026730327919489892 -0.0041190678172986755 -0.04514848676152181; 0.021530197479120935 -0.003289006486758767 -0.062176229612947755; 0.016667212026538644 -0.003597917260590619 -0.06423597677806316; 0.01702421025810688 -0.005223207547535032 -0.08087285152444403; 0.011747901478544442 -0.004227676260266376 -0.06508255681444254; 0.017058252720700447 -0.007888190206629666 -0.10327856559219219; 0.014648343592666748 -0.0079134643571973 -0.09411568962894719; 0.024087415186466152 -0.01196112431792353 -0.1518922946256035; 0.0339013932746406 -0.0255689214773916 -0.22682234234377072; 0.003406941284632415 -0.002296454660454965 -0.024379387335030003; 0.00015108784429228677 0.00015452107259769285 -0.0006549470186123287; -3.0269149714549126e-6 0.00030623624480393996 -0.0011686032752905653; 0.00020564323193064758 -5.733851643281113e-5 -0.00039687998160512774; 0.0002579694485170279 0.0005731068505990453 0.0005293325499666453; -0.0006953745318426922 0.0002777493201572389 -0.00023570481164811167; -0.0002458967064193549 0.00014452977296441699 0.000595461296313574; -0.00011570096772836876 -0.0003212608611051738 0.0006305582981858433; -0.00014834889010926507 0.0002118491319052627 0.0004642277022704265; 2.3796912148285154e-5 1.7603435499634714e-6 -7.800225841518376e-5] %
|
|
|
|
Mass Used: 75.68964180961575 kg
|
|
Launch C3: 102.3419700357316 km²/s²
|
|
||V∞_in||: 2.337318311731968e-6 km/s
|