NWPU tested a combined cycle SCRAM engine on July 4th.
其成功发射在国际首次验证了煤油燃料火箭冲压组合循环发动机
火箭/亚燃、亚燃、超燃、火箭/超燃的多模态平稳过渡和宽域综合能力,突破了热力喉道调节、超宽包线高效燃烧组织等关键技术,飞行试验圆满成功。
The engine uses kerosene as fuel. It went through mode transition from Rocket (boosted) RAM to RAM (booster seperated) to SCRAM to
rocket (assisted) SCRAM.
It is worth to note that one of the institutes besides NWPU in the project is 北京动力机械研究所/Beijing Power Machinery Institute (BPMI) which proposed TRRE in a paper in 2017.
The TRRE engine uses turbine for horizontal take off. Either BPMI is working on two different combined cycle engines or this NWPU test is one of the tests to verify the high mach flight of TRRE.
The reason that I suspect this test may be related to TRRE is that final stage of the test is in rocket/scram mode. Since the booster has been dropped, the only rocket involved must be inside or part of the engine. And the rocket can not be large because it is only involved in the highest speed range of the engine. This flight mode is described in the paper.
The paper also laid out the road-map as "building flyable engineering prototype before 2025". Since the 0 to 1.8M regime is easy and likely already tested, successfully testing the ram and scram regime in 2022 seems to fit very well with the road-map.
BTW, the paper is titled "Analysis of Key Technologies and Propulsion Performance Research of TRRE Engine".