【天火三号试车成功,建议公司下次换个好点的摄像头】北京天兵科技自主研制的国内首台30吨推力HCP火箭发动机天火三号(TH-3)全系统热试车取得成功。
12月以来,TH-3发动机共进行了6次稳态程序的考核,发动机启动、关机平稳,稳态工作参数正常,发动机各项性能指标均达到了设计要求,全面通过热试车考核。
天火三号30吨级发动机是继天火一号(1000N)全系统热试车、天火二号(10000N)全系统热试车成功研制的基础上,由天兵科技独立自主研发生产的,是目前世界上HCP推进剂体系中推力量级最大的发动机,从设计到生产、再至试验点火成功,历时一年,发动机主要零组件采用3D打印方案,发动机研制过程中借鉴了液体火箭发动机和固体火箭发动机交叉融合的设计经验,进行了大量首创性的精密结构、新材料、新工艺的工程应用,提高产品可靠性的同时,大幅降低了发动机生产成本。
天兵科技称,HCP推进剂是航天领域内公认的先进液体推进剂体系,具有绿色无毒、常温贮存、高性能(公司未公开TH3的比冲水平,但以NOFBX相关论文称,比冲可以高到325s,远在单组元发动机之上,甚至超过传统肼基推进剂)、低成本、系统简洁可靠性高的特点。天火三号发动机的试车成功,标志着该推进剂体系的研究已进入工程化应用阶段。采用HCP推进剂的天火三号发动机具备了传统低温双组元推进剂的高性能,同时具备了单组元发动机的可靠性和使用便捷性。这意味着,装备天火三号发动机的液体运载火箭较同等运力规模的火箭,起飞重量降低50%、零部件数量减少60%,大幅降低了运载火箭的制造和发射成本,同时显著提升了运载火箭的可靠性,是未来低成本、高频次进入太空的优质解决方案。此外,得益于天火发动机先进的设计理念和HCP推进剂体系的特点,天火系列发动机还具备连续深度变推力能力,能够让火箭更容易实现回收复用功能。
现在是点评时间,这个HCP应该是一种预混合的推进剂,国外叫NOFBX。绿色无毒比冲相对高,听起来很美,但国内外不大力推进是有原因的,有一定危险性。此类发动机国内外试车时都炸过台子,这种发动机在关闭时控制不好容易回火,沿着燃烧室往上烧,因为推进剂本身就是混合好的。
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Space Enthusiast Network
Today at 10:00 from Weibo video
Beijing Tianbing Technology independently developed the first domestic 30-ton thrust HCP rocket engine Tianhuo III (TH-3) full system hot test successfully.
Since December, the TH-3 engine has undergone a total of 6 steady-state program assessments. The engine starts and shuts down smoothly, and the steady-state working parameters are normal. The engine's performance indicators have reached the design requirements and fully passed the hot test.
The 30-ton engine of Tianhuo-3 is developed and produced by Tianbing Technology independently following the successful development of Tianhuo-1 (1000N) full-system hot test run and Tianhuo-2 (10000N) full-system hot test run. It is currently the largest thrust HCP propellant engine system in the world. From design to production, and then to the successful test ignition, it took one year. The main components of the engine used 3D printing. The design experience of the cross-fusion of liquid rocket motors and solid rocket motors was used for reference in the engine development process. A large number of pioneering engineering applications of precision structures, new materials, and new processes have been carried out to improve product reliability and greatly reduce engine production costs.
Tianbing Technology claims that HCP propellant is a recognized advanced liquid propellant system in the aerospace field. It has green, non-toxic, room temperature storage, and high performance (The company has not disclosed the specific impulse level of TH3, but according to NOFBX related papers, the specific impulse can be as high as 325s, which is far higher than that of other mono-propellant engine and even more than traditional hydrazine-based propellants), low cost, simple system and high reliability. The successful test run of the Tianhuo-3 engine indicates that the research on the propellant system has entered the engineering application stage. The Tianhuo-3 engine with HCP propellant has the high performance of traditional cryogenic bi-propellant, and at the same time has the reliability and convenience of mono-propellant engine. This means that the liquid launch vehicle equipped with the Tianhuo-3 engine has a 50% lower take-off weight and a 60% reduction in the number of parts than a rocket of the same capacity, which greatly reduces the manufacturing and launch costs of the launch vehicle, and at the same time significantly improves the reliability of the launch vehicle. It is a high-quality solution for low-cost, high-frequency entry into space in the future. In addition, thanks to the advanced design concept of the Tianhuo engine and the characteristics of the HCP propellant system, the Tianhuo series of engines also have the ability for continuous throttleability, which can make it easier for the rocket to realize the recovery and reuse function.
Here is the time for comment (Note: from editor of Space Enthusiast Network).
This so-called HCP should be a pre-mixed propellant, called NOFBX abroad. Green and non-toxic, the specific impulse is also relatively high, sounds wonderful. But there are reasons why domestic and foreign efforts are not vigorously pursue. There is a certain risk. This type of engine has a history of explosion during test runs at home and abroad. This kind of engine is not easy to control during turn off, when it could backfire and burn up along the combustion chamber because at that time the propellant is already well mixed.
Video link of the test ->
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