A rocket-based combined-cycle (RBCC) engine synthetically integrates a traditional rocket
engine with an airbreathing engine, effectively combining both advantages of high thrust-to …

Rocket-based combined-cycle (RBCC) engines are known as the most promising type of
engine with the potential to realize 'single stage to orbit'(SSTO). This will dramatically reduce …

As the inflow velocity increases, rocket-based combined cycle (RBCC) engine typically
require a ramjet/scramjet mode transition within the flight range Ma∞= 5.5 to 6.0. However …

This paper expounds on the development status and relevant works of control and guidance
methods of the aerospace vehicle in recent years. The control difficulties and the solutions in …

The rocket-based combined-cycle (RBCC) engine usually completes the transition process
from ramjet to scramjet mode under the Ma∞= 5.5–6.0. The dual-mode (ramjet/scramjet) …

Direct thermoelectric conversion is a promising technology that converts aerodynamic and
combustion heat into electric energy for thermal management of supersonic combustors …

Flow separation and transitions of separation patterns are common phenomena of nozzles
working with a wide Mach range. The maximum thrust method is applied to design the single …

Aiming at ascent trajectory planning of pre-cooled combined power vehicles, in order to
ensure the optimal flight performance of pre-cooled combined power engines, the paper …

With the development of the next generation of reusable aerospace vehicle, the technique of
the Rocket Based Combined Cycle (RBCC) engine becomes increasingly significant and …