— Ch. 1 · Fundamental Physics And Theory —
Spacecraft propulsion.
~6 min read · Ch. 1 of 6
A remote camera captures a close-up view of an RS-25 during a test firing at the John C. Stennis Space Center in Hancock County, Mississippi. This image represents the tangible reality behind abstract equations that govern all spacecraft motion. The Tsiolkovsky rocket equation shows that for a rocket engine to change momentum, it must exhaust mass opposite the acceleration direction. Both reaction mass and energy are required for this process to occur. In conventional solid or liquid rockets, fuel is burned to provide energy while reaction products flow out of the nozzle as propellant. Ion thrusters use electricity to accelerate ions behind the spacecraft instead. Here other sources like solar panels or nuclear reactors provide electrical energy while ions serve as reaction mass. The rate of change of velocity is called acceleration and the rate of change of momentum is force. To reach a given velocity one can apply small acceleration over long time or large acceleration over short time. For maneuvering in space tiny accelerations over long periods often produce same impulse as large forces over short durations. However when launching from a planet tiny accelerations cannot overcome gravitational pull so they cannot be used.
Chemical Propulsion Systems
Bipropellant rocket engines of the Apollo Lunar Module reaction control system demonstrate decades of chemical propulsion evolution. A large fraction of rocket engines today obtain thrust by chemical reactions creating hot gas expanded through bell-shaped nozzles. Many different propellant combinations include hydrazine, liquid oxygen, liquid hydrogen, nitrous oxide, and hydrogen peroxide. These fuels work as monopropellants or bi-propellants depending on mission requirements. Rocket engines generally produce high-temperature reaction mass as hot gas achieved by combusting fuel with oxidizer within combustion chambers. Exhaust speeds reaching ten times speed of sound at sea level are common for these systems. The dominant form of chemical propulsion for satellites has historically been hydrazine but this fuel is highly toxic. Non-toxic green alternatives are now being developed to replace hydrazine globally. Nitrous oxide-based alternatives are garnering traction and government support with development led by Dawn Aerospace, Impulse Space, and Launcher. The first nitrous oxide-based system flown in space was D-Orbit onboard their ION Satellite Carrier in 2021 using six Dawn Aerospace B20 thrusters launched upon SpaceX Falcon 9 rockets.