missions/nlp_1_phase---------------------------

Spacecraft: bepi
	dry_mass: 2000.0 kg
	specific impulse: 2800.0 kg/s
	max_thrust: 0.0005 kN
	num_thrusters: 2
	duty_cycle: 0.9
Launch Mass: 3600.0 kg
Launch Date: 1992-11-12T00:00:00.012
Launch V∞: [9.677342245913248, 1.2148911343904845, 1.4770002664775748] km/s
Phase 1:
	Planet: Venus
	V∞_in: [9.995477533479665, -4.770529222466886, -1.7643262560938888] km/s
	V∞_out: [4.542216161608705, 0.1169383121147722, -0.5297547896681116] km/s
	time of flight: 1.0342080018919956e7 seconds
	arrival date: 1993-03-11T16:48:00.012
	thrust profile: [-0.06827956587597055 0.2189651579368032 0.22260889586646854; -0.5657492453559373 0.08687547481531692 0.09138393271069822; -0.7627133026838161 0.04522025084077273 0.06051223750173192; -0.8694853207917537 0.004020122983347096 0.04412034762690886; -0.9156699467684505 -0.05071240769308274 0.03110069387793629; -0.9307669202914396 -0.1219964600790567 0.01923669861767808; -0.9342334366509295 -0.20780403813377482 0.0078030080771221266; -0.9355559722321648 -0.30276368006072857 -0.0035345858246075956; -0.938210990244296 -0.39973779814825156 -0.014841057433864407; -0.9428326748546626 -0.4922801244635121 -0.025964447511107023; -0.948952802856955 -0.5759010541594941 -0.036681448092579935; -0.9557798460559065 -0.6474598520145747 -0.04675072941621921; -0.962549888811903 -0.7047205371292298 -0.055638699294433915; -0.9686622563853547 -0.7463664783144444 -0.0625857936749166; -0.9737612697271567 -0.7715231321565172 -0.06659149605871661; -0.9777967996020939 -0.7783020776379241 -0.06623218175189496; -0.9810653384331429 -0.7604447108250885 -0.0594729767608653; -0.9842857104464896 -0.7004371830045492 -0.04358728653836779; -0.9887220681198762 -0.5548364920968362 -0.01489473159954481; -0.9966878745813371 -0.2184651547964285 0.03090315333337913] %

Mass Used: 380.34886252983915 kg
Launch C3: 97.30844320013269 km²/s²
||V∞_in||: 11.215184676261444 km/s