Explore: *combustion Stability

desirable propellants because they have reasonably high density and their combustion products have high specific impulse (Isp). This allows the volume of the

internal combustion engine (ICE or IC engine) is a heat engine in which the combustion of a fuel occurs with an oxidizer (usually air) in a combustion chamber

economy and emissions performance by reducing engine knock, improving combustion stability and controlling injection more precisely. Production ended in 2024

problem during combustion that would sometimes cause catastrophic failure. In October, 1962, Dr. Klute presided over the Combustion Stability Committee at

known as a sidevalve engine or valve-in-block engine, is an internal combustion engine with its poppet valves contained within the engine block, instead

evaluated by Rocketdyne for possible upgrades to the SSME. It achieved combustion stability without the acoustic resonance chambers that the SSME required. Thrust

bipropellant rocket engine. In this cycle, the fuel is used to cool the engine's combustion chamber, picking up heat and changing phase. The now heated and gaseous

duration and timing. The new MIVEC system together with improved combustion stability and a reduction in piston friction provide an improvement in fuel

specific impulse. The aluminium improves specific impulse as well as combustion stability. High performing propellants such as NEPE-75 used to fuel the Trident

The Wankel engine (/ˈvʌŋkəl/, VAHN-kəl) is a type of internal combustion engine using an eccentric rotary design to convert pressure into rotating motion