The 500-ton liquid oxygen rocket engine, developed by China Aerospace Science and Technology Corporation made a breakthrough on Fri with a successful full working condition trial. The engine has three times the thrust power of 200-ton engine, and is at the global advanced level.
I am not sure about that part although I don't have the inside information to back up my thinking. The wording was "全工况半系统" "full working condition half system". If not igniting the mix, the pre-burner would not be run, the chamber pressure, temperature and ignition sequence would not be tested. It is hardly a full working condition.View attachment 69513
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New 500 ton class hydrolox engine intended for super heavy launch vehicle. Successful full duration half system test (I'm guessing running the turbopumps but not igniting the mix). Most powerful dual combustion chamber rocket engine in the world currently.
Compared to 120 ton staged combustion hydrolox engine (must be YF-100):
3 times more thrust (I understand that as equal to thrust of four YF-100)
3% better specific impulse
25% better thrust to weight ratio:
So in my book that works out to be 309s Isp at sea level, 80 TWR. It's basically a Chinese RD-180, slightly better TWR, slightly worse Isp. Excellent first stage engine for moonshot rocket by any measure.
3月25日下午,“天鹊”(TQ-12)80吨液氧甲烷发动机半系统联合试验圆满成功,试验数据表明设计方案可靠、产品性能稳定。
半系统点火试车在蓝箭航天热试车台进行,试验装置包括除推力室之外的涡轮泵、燃气发生器、各种阀门、点火和起动装置以及总装管路,所有核心部组件的稳定性均一次性通过考核。试验的成功验证了涡轮泵和各种阀门的设计和工艺方案的可行性、系统的协调性和匹配性、起动时序的正确性,为整机试车奠定了基础。
What do you mean? Tianwen-1 is a satellite of Mars. The previous NASA MRO (Mars Reconnaissance Orbiter) and ESA Mars Express are all satellites.It's never occurred to me if there are satellites orbiting Mars.
I know, it's incredibly obvious that there would be some. My dumb brain just never thought about satellites aside from flybys. One of those embarrassing knowledge gaps.What do you mean? Tianwen-1 is a satellite of Mars. The previous NASA MRO (Mars Reconnaissance Orbiter) and ESA Mars Express are all satellites.
Indeed my bad, it's kerolox, hence comparison to RD-180 and YF-100.@Temstar
Surely you must mean kerolox not hydrolox. 300 Isp is too low for a hydrogen engine. Even methane should have more Isp.
I assume this was a test where they ran the engine turbopumps with water to check if they have enough performance.
No. The turbine is for two pumps and two chambers, if the turbine runs full power, there has to be either two chambers burning all the fuels (for two chambers) or not burning any but using water to test the pumps only.Could the '全工况半系统"' means the rocket engine designed with 2 burn chambers like the Russian but only installed and fired with 1 chamber (half system) during the test?