23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5631307715394686---------------------------
|
|
|
|
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: 2023-04-30T11:07:18.323
|
|
Launch V∞: [6.557143169616849, -7.354367867812205, 0.10542111366833992] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0005563585477661404, -0.0035875812496256793, 0.0050682666848637144] km/s
|
|
V∞_out: [-0.004345872234195327, -0.0033700890429713875, -0.0026623785533602994] km/s
|
|
time of flight: 1.8749577787504765e8 seconds
|
|
arrival date: 2029-04-08T13:16:55.323
|
|
thrust profile: [0.2205900075591794 -0.051093597578176574 -0.07257099536144586; 0.13165042045502284 0.04095036593153822 -0.12816404018377284; 0.0751217056556292 0.04400707667510081 -0.12450980817188409; 0.05587372194491444 0.044231087397493554 -0.13071770442668226; 0.037660477953556266 0.03635920191596844 -0.11504751093893452; 0.022565172079590304 0.02466777033292644 -0.08485021447850843; 0.018331559210325265 0.022540222560408534 -0.08181660301672118; 0.012522316329328013 0.017132886886730682 -0.0678808247059965; 0.005367205468760105 0.009461510745108911 -0.031199778792044233; 0.002197319639930971 0.003449839507681004 -0.014575841493839147; 0.0026793272272000205 0.0065314360415946555 -0.029472481913019967; 0.0021349495615814807 0.004056723261955454 -0.016218079218086764; 0.0005727976766788062 0.0002702873352729543 -0.0009100098120564236; -0.00018951531333639358 8.462901672718379e-5 0.0009678053637633176; -0.0009568524669531003 -0.0008409176461969723 -0.0003138714726482648; -0.0017430626393532358 0.0018519767424252096 -4.951648571186373e-5; -0.00034102820663015076 0.0016217727027047846 0.001680390593833812; 0.0008627899331875465 -0.00023407320233373286 -0.00019401398631564725; -0.0015654338971001214 -0.002069316310499582 0.00015165161517515413; 8.00025046984761e-5 0.0010450224900271964 0.0039037366675530585] %
|
|
|
|
Mass Used: 90.60442658589636 kg
|
|
Launch C3: 97.09396689316863 km²/s²
|
|
||V∞_in||: 0.006234388602360108 km/s
|