SYS_EXTRACTION_INIT
DOWNLINKING VECTOR PARAMETERS
DECRYPTING CORE ALGORITHMS...
DECRYPTING CORE ALGORITHMS...
Audit the mission. Calculate the maximum change in velocity (Delta-V) of a spacecraft stage based on specific impulse and mass ratio.
To reach Low Earth Orbit (LEO), a rocket needs approximately 9.4 km/s of Delta-V. At your current mass ratio and efficiency, you can achieve 6.77 km/s. This logarithmic relationship is why multi-stage rockets are required for deep-space exploration.