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			2.0 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
			
		
		
	
	
			23 lines
		
	
	
		
			2.0 KiB
		
	
	
	
		
			Plaintext
		
	
	
	
	
	
| archive/ES_0.5826361699973581---------------------------
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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: 2023-04-20T00:02:12.672
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| Launch V∞: [6.44609305640883, -6.903383053903391, 0.7607070831878705] km/s
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| Phase 1:
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| 	Planet: Saturn
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| 	V∞_in: [0.012747443163675926, -0.005762894169105177, 0.015205678378701801] km/s
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| 	V∞_out: [-0.013127743904503124, -0.00582465536238911, -0.014839191615511152] km/s
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| 	time of flight: 1.8749577787479886e8 seconds
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| 	arrival date: 2029-03-29T02:11:49.672
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| 	thrust profile: [1.0 -0.23759439685349074 -0.14516219382367962; 0.25279096150086255 0.10220981956427366 -0.15037666699668378; 0.09346322669187135 0.07244220481898014 -0.10450064733189499; 0.08071676981048524 0.08801802902368132 -0.13032966291162107; 0.05619258248760819 0.07688403512267325 -0.11932197540427913; 0.046234431503934206 0.07865785765333844 -0.1156080031556485; 0.009120020752835162 0.01735314454913359 -0.030113622664211238; 0.010346874151251457 0.01981566369234821 -0.03692838921136083; 0.0023593155152211664 0.007152083057680791 -0.012396224002779633; 0.0010185379236728066 0.0027457200737959478 -0.005631183405987826; 0.00012197336009117204 0.0006666549381236434 -0.0011024126169497301; 5.1488192269217073e-5 -1.163540400123689e-5 0.00022659838473745332; -0.00032621427488147237 0.00014834532982351613 -0.00046738966825997656; 0.0002553521643373153 1.7332157903336798e-5 -0.0003337297720705001; 0.00029974771370480495 0.00032500183563790685 -0.0005460282069383875; -0.0002333727163445265 3.503219949458814e-5 -0.0004203284560941256; 0.00017286535217015496 -9.235699822854775e-5 1.351593728623663e-5; 0.0002704182638864422 0.00032423770251867453 0.00018561573742097195; -0.00018953230939764136 -0.00010268854284177159 -1.9501281501539742e-5; -0.00016337323160921138 -0.00016433768523096005 0.0007253796938918001] %
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| 
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| Mass Used: 155.98184847149787 kg
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| Launch C3: 89.78748854721485 km²/s²
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| ||V∞_in||: 0.0206620645476674 km/s
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