01
Rocket Propulsion
Rockets generate thrust by expelling mass and conserving momentum. They can operate in vacuum because they do not require atmospheric oxygen for the fundamental momentum-exchange mechanism.
F ≈ ṁv_e + (p_e-p_a)A_e
02
Specific Impulse
I_sp = F/(ṁg₀)
Specific impulse is a measure of propulsion efficiency in terms of thrust produced per unit weight-flow rate of propellant.
03
Electric Propulsion
Electric propulsion accelerates propellant using electrical energy and can achieve high exhaust velocities. Its limitation is generally low thrust compared with chemical propulsion, making it useful primarily for gradual trajectory changes.