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			2.0 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
			
		
		
	
	
			23 lines
		
	
	
		
			2.0 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
| archive/ES_0.5950873272306814---------------------------
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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: 2023-04-23T02:03:18.064
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| Launch V∞: [5.090267173313352, -8.353082632733752, -1.0569531543947648] km/s
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| Phase 1:
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| 	Planet: Saturn
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| 	V∞_in: [-1.609382630001616e-5, 1.0536146903114536e-5, -2.197691424951296e-5] km/s
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| 	V∞_out: [-2.078035498740908e-5, -1.8363406702493447e-5, -9.09735309777092e-6] km/s
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| 	time of flight: 1.3019759502743064e8 seconds
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| 	arrival date: 2027-06-08T00:03:13.064
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| 	thrust profile: [0.7017384188284962 -0.4721624908798447 -0.36179124264389256; 0.22003757074643038 -0.02899414229738172 -0.24330451348141424; 0.10208157808046613 0.007177970364539154 -0.17111948141106187; 0.08456065166898062 0.015863695723201524 -0.18500874292835195; 0.08622873242341877 0.022945758780129808 -0.22746676477884933; 0.06876614555855895 0.022123658554953955 -0.2100490899737593; 0.01906161419375614 0.007054136162734147 -0.06717363776408819; 0.03417292064073816 0.01381510106959681 -0.12941986854896637; 0.0038300464516790077 0.0006226095003240219 -0.01955383993417543; 0.00434952552815527 -0.0032836581709765043 -0.021272419268462503; 0.0018594262285659196 -0.00021756315274225162 -0.014937723505245684; 0.004411362596379011 0.001708335808645344 -0.012953237730027265; 0.006136184497856283 0.0012012535557659153 -0.027977443568746718; 0.01664740071612785 0.004174780575169212 -0.015823795301086373; -0.0020904521817622064 -0.0005069306186709325 0.0043562399474371205; -0.0009607186746955008 -4.7404131656434475e-5 0.0019233729676209066; 0.002503482237466637 -0.0057032715879500664 -0.0033851906361304276; 0.000615202884347989 -0.0031335977376583616 -0.00897645701898867; -0.0031690385231792767 -0.001258639220228497 0.004257159512146717; -0.0002291292680820209 0.0003205415483476127 -0.023930196320259556] %
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| 
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| Mass Used: 129.59045231160871 kg
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| Launch C3: 96.80195933557478 km²/s²
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| ||V∞_in||: 2.9206273238288167e-5 km/s
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