Sökning: "Hybrid Rocket"
Visar resultat 1 - 5 av 11 uppsatser innehållade orden Hybrid Rocket.
1. Design and Implementation of a Rocket Launcher Hybrid Navigation
Master-uppsats, KTH/Lättkonstruktioner, marina system, flyg- och rymdteknik, rörelsemekanikSammanfattning : Rocket Factory Augsburg (RFA) a German New Space Startup is developing a three-stage rocket launcher aiming at LEO/SSO orbits. A fundamental responsibility of the GNC team is the development of the rocket navigation algorithm to estimate the attitude, position, and velocity allowing the guidance and control loops to autonomously steer the rocket. LÄS MER
2. Simulation of Combustion in a Hybrid Rocket Engine
Master-uppsats, KTH/Skolan för teknikvetenskap (SCI)Sammanfattning : A numerical investigation on the combustion mechanics of a hybrid rocket engine is performed through unsteady Reynolds-averaged Navier-Stokes simulation. The hybrid rocket engine model is based on an experimental laboratory scale engine design operating on GOX and HDPE as a propellant. LÄS MER
3. Design of a modular small-scale PMMA/Air hybrid rocket research engine
Master-uppsats, Luleå tekniska universitet/Institutionen för system- och rymdteknikSammanfattning : Rocket propulsion using the hybrid-propellant scheme is a technology that offers much promise in applications where high-performance liquid rocket engines are deemed too complex and solid rocket motors are considered to lack performance or safety. However, despite extensive research, there is still a lack of knowledge in the theoretical aspects of hybrid rocketry, especially in the area of fuel-oxidizer mixing and fuel regression rate. LÄS MER
4. Parametric study on hybrid rocket propulsion system performance measured by the system specific impulse
Master-uppsats, Luleå tekniska universitet/Institutionen för system- och rymdteknikSammanfattning : Hybrid rocket motors have become of great international interest during the last couple of years. A hybrid rocket motor is propelled by the use of a solid fuel and a liquid oxidizer. The fundamental principle of the hybrid propelled system is that the liquid oxidizer is injected into a combustion chamber to enable the combustion of the solid fuel. LÄS MER
5. Formulation and Assessment of Hexamethylene-tetramine Filled Solid Fuel Grains
Master-uppsats, KTH/Fiber- och polymerteknologiSammanfattning : Hybridraketer har inte sett så mycket användning som dess motsvarigheter som använder flytande eller fasta drivmedel. De främsta orsakerna kan förklaras med att hybridraketer historiskt sett haft lägre regressionshastighet och bränsletäthet. Inverkan av nackdelarna har dock minskat tack vare fortsatt forskning rörande hybridraketer. LÄS MER