23 lines
		
	
	
		
			2.0 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
			
		
		
	
	
			23 lines
		
	
	
		
			2.0 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
| archive/ES_0.6600318417630374---------------------------
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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: 2024-05-09T20:50:15.043
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| Launch V∞: [7.440751611047492, -7.6801114087868845, -2.1601082699767433] km/s
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| Phase 1:
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| 	Planet: Saturn
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| 	V∞_in: [0.5475198594096093, -0.5103231919669784, -0.058258516311550455] km/s
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| 	V∞_out: [0.4833649118444065, -0.39615859990399227, 0.41638463085007543] km/s
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| 	time of flight: 9.684612874924362e7 seconds
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| 	arrival date: 2027-06-04T18:32:23.043
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| 	thrust profile: [0.6163632836856306 -0.3294352013215769 -0.34936810840575117; 0.3227096945791794 -0.035470120915439544 -0.3323724328346466; 0.14708444811577626 0.009747107014753526 -0.22141011846133624; 0.09030622611179712 0.014366267605606964 -0.17328119070309095; 0.05431213951587406 0.011626525306337974 -0.12379113680578895; 0.019649230818070438 0.004739102079948441 -0.05141793552777896; 0.005320448343216786 0.001941392584108716 -0.01609666616223926; 0.0013024246741111054 0.0018225152439931371 -0.007493406726467794; 0.0010844912187936706 -0.0007411816951612908 -0.008613411389893355; -0.0005328384707675281 0.001924407786207076 -0.003938821282854829; 0.0016505133301074931 0.000405781741715657 -0.006976952293655454; -1.024499741957512e-5 -0.0006318430336174979 8.98417031861506e-5; -0.0015730126283751544 0.0008325178931937819 -0.0007996514527554932; 0.0007642603302840707 -0.001019744952815311 0.0002134955090882316; -0.00019291786698636196 -0.0007143767342952191 -0.003234827620019687; 0.00031780821465164665 0.0005719948198019603 -0.0018232218619964919; -0.0018519344139045428 -0.00013291580905844995 0.0014734349446017597; -0.0011897701223931877 3.996163567011388e-5 0.0005453008144694413; 0.00010319768700919494 0.0028957344820051247 -0.0011072429848282335; 0.0002551461628100339 -0.0013957870084395866 -0.005052712510771773] %
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| 
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| Mass Used: 75.78319481775725 kg
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| Launch C3: 119.01496352670624 km²/s²
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| ||V∞_in||: 0.7507341816049853 km/s
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