SYS_EXTRACTION_INIT
DOWNLINKING VECTOR PARAMETERS
DECRYPTING CORE ALGORITHMS...
DECRYPTING CORE ALGORITHMS...
Audit your mission capability. Calculate the total change in velocity (Delta-v) achievable based on the Tsiolkovsky rocket equation and propellant mass fraction.
Delta-v is the "fuel" of space travel. To reach Low Earth Orbit (LEO), you typically need a total Delta-v of 9,400 m/s (including atmospheric losses). This audit highlights the extreme mass fraction required for interplanetary flight.