23 lines
		
	
	
		
			2.0 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
			
		
		
	
	
			23 lines
		
	
	
		
			2.0 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
| archive/ES_0.7108735196419596---------------------------
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| 
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| Spacecraft: mySat
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| 	dry_mass: 200.0 kg
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| 	specific impulse: 3200.0 kg/s
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| 	max_thrust: 0.00025 kN
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| 	num_thrusters: 1
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| 	duty_cycle: 1.0
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| Launch Mass: 3500.0 kg
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| Launch Date: 2023-04-26T08:59:16.010
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| Launch V∞: [6.636120312355136, -9.062835074600471, -2.5129528716276797] km/s
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| Phase 1:
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| 	Planet: Saturn
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| 	V∞_in: [-0.07453967522605967, 0.050968624014962625, 0.09420481357635103] km/s
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| 	V∞_out: [-0.04237940814409329, 0.08963547110402116, -0.08484493061985303] km/s
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| 	time of flight: 8.812229936581476e7 seconds
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| 	arrival date: 2026-02-09T07:24:15.010
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| 	thrust profile: [0.5706093050976743 -0.43256646614565725 -0.2769840695409991; 0.2206316734117003 -0.06088997570344648 -0.17163073454226963; 0.0599420079170459 -0.0050082681759998785 -0.06590546378762228; 0.0416786992272192 0.0016509888613389062 -0.053323540972976625; 0.066406223736814 0.006123976253426823 -0.10073301058332118; 0.04091144720793393 0.0034299700507539692 -0.06831431497194548; 0.0037327425759777384 0.0031081077294287797 -0.004137817556081025; 0.0061312766193650885 0.00022633224662385793 -0.011326690412420667; -0.0029033438395254575 -0.002519058168409026 -0.0015124209518248511; -1.4204108351099226e-5 0.00033796844136307143 -0.002312991244180997; 0.006625817485535977 0.0019180961611494384 -0.0005238779753748716; -0.004447011778851783 -0.0006086067788897166 0.007106137437403626; 0.0012002633265303716 -0.0056565563805537275 -0.011200621116457803; -0.02558412767410058 0.004383528251754068 -0.007120700860011395; 0.0007171771356153619 0.0012023430054972676 -0.0062130023896693285; 0.016467644903038144 -0.015123508810938754 0.013943645804738565; 0.0009464092103305946 -0.00013178824141531513 0.002462174690735573; -0.022857703490786526 0.0046221119555822955 0.028160842673622583; -0.014175201041075766 -0.0036136290719581752 0.029106176933656712; -0.007997716818450362 0.0035454859891463817 0.01092762967038463] %
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| 
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| Mass Used: 56.50574652280329 kg
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| Launch C3: 132.48800452448276 km²/s²
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| ||V∞_in||: 0.13049333591314205 km/s
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