archive/ES_0.582673933161944---------------------------

Spacecraft: mySat
	dry_mass: 200.0 kg
	specific impulse: 3200.0 kg/s
	max_thrust: 0.00025 kN
	num_thrusters: 1
	duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2024-05-23T07:46:00.025
Launch V∞: [7.521776502096289, -6.694752764578151, -0.3437999744703748] km/s
Phase 1:
	Planet: Saturn
	V∞_in: [5.473405863030035e-6, -0.00036811126126213406, -6.352145644263261e-6] km/s
	V∞_out: [-0.0003560909361638837, 5.197276732271308e-5, -7.910038075024872e-5] km/s
	time of flight: 1.87495777809551e8 seconds
	arrival date: 2030-05-02T09:55:37.025
	thrust profile: [0.3007522384645069 0.01538459091673179 -0.11131327349380553; 0.10462906943309809 0.05936558513943002 -0.12192367684619146; 0.04883762727291934 0.04194968734000627 -0.10071734456768278; 0.0625276463759093 0.08036307981441099 -0.19579718604034607; 0.025160981451941435 0.032005353163988066 -0.09993203581442411; 0.019703142299311974 0.028777060045858723 -0.09820301977209817; 0.004260927447670723 0.005826439344016362 -0.025059989250901207; 0.0034365142414651178 -0.0006297203077354665 -0.004964275505617658; 0.0022540085785221916 0.0035724439346107423 -0.004044480929815054; -0.005524746142926255 0.002809523645799304 -0.0038359643301211508; -0.000541347593971556 -0.00010606903075146624 -0.0025465081760385924; 0.002706331495536553 0.008217032647852635 -0.0027368588476257864; 0.0008973650128930848 0.0004370531612664909 -0.00611219902562141; 0.003181603673715017 0.004103545933158068 -0.005537514875076723; 0.00018584808398951962 -0.008575096194707562 -0.005651574056551431; 0.001925012936609219 0.0028970395102776267 -0.010625765732168602; 0.0002708462384359184 0.0006423975171832652 -0.007075401356268291; -0.011781773885935298 0.004500983379803739 -0.007827735621928983; 0.005066062809248608 0.009226874288704986 -0.008876237302336668; 0.0002970940320755893 -0.0003046324543979977 0.0008236788280938921] %

Mass Used: 87.61521932116511 kg
Launch C3: 101.51503474876051 km²/s²
||V∞_in||: 0.0003682067470783588 km/s