For SSTOs, the system must include a rocket engine for the end of the flight, outside atmosphere. a. One of the most studied cycles is the turboramjet: The turbojet is located inside the ramjet. It is used in turbo mode first, then undergoes a transition at around Mach 3. It globall...
Experimental studies pertinent to axisymmetric, sudden-expansion dump combustor configurations for integral rocket-ramjet missiles have been performed under cold flow test conditions. These studies have included surface flow visualizatio... James,E.,Drewry - 《Aiaa Journal》 被引量: 101发表: 1977年 ...
Historically, rocket-based propulsive systems have been utilised for the purpose of propelling aircrafts and spacecrafts to hypersonic flight speeds. However, air-breathing modes of propulsion tend to be preferable for sustained atmospheric flights due to their virtue of operation without the necessity ...