SYS_EXTRACTION_INIT
DOWNLINKING VECTOR PARAMETERS
DECRYPTING CORE ALGORITHMS...
DECRYPTING CORE ALGORITHMS...
Audit the air. Calculate the pressure, temperature, and density (rho) of the atmosphere at any altitude using the International Standard Atmosphere (ISA) model.
At 11000 meters, the air is only 30% as dense as at sea level. This reduction in density reduces lift but also significantly lowers aerodynamic drag, enabling high-speed cruise flight.