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TH-12

From Wikipedia, the free encyclopedia
TH-12
Country of origin China
Manufacturer Space Pioneer
Status Under development
Liquid-fuel engine
Propellant LOX / RP-1
Performance
Thrust, vacuum 1,350 kilonewtons (300,000  lbf )
Thrust, sea-level 1,090 kilonewtons (250,000  lbf )
Throttle range 40%~110%
Thrust-to-weight ratio 163
Specific impulse , vacuum 335s
Specific impulse , sea-level 285s
Used in
Tianlong-3
References
Notes [1]

The TH-12 ( Chinese : 天火-12 ; pinyin : Ti?nhu?-12 , lit. Sky Fire 12 ) is an oxidizer-rich gas-generator cycle rocket engine burning LOX and kerosene under development by Space Pioneer . The TH-12 utilizes 3D printing and has the highest target thrust among all commercial rocket engines in China. The engine features deep throttling for reusability, re-ignition, thrust vectoring , and multi-mode starters. [2]

History [ edit ]

Space Pioneer proposed the TH-12 engine for its Tianlong-3 launch vehicle. [3] Engine development was underway in December 2020, with the first gas generator test performed in September 2022. In November 2022, a full-stage developmental TH-12 engine successfully completed its first static fire test. [4]

On July 24, 2023, the TH-12 engine, in the flight configuration of the first Tianlong-3 rocket, successfully completed a full-duration hot fire test at rated conditions for a single burn duration of 100 seconds, accumulating a total test duration of 200 seconds. This test demonstrated that the engine met the flight requirements for the Tianlong-3 rocket. [5]

In early January 2024, the TH-12 engine completed a calibration hot fire test for the first flight batch, subjecting the engine to a 50-second process verification test at rated conditions, demonstrating rapid startup, smooth operation, and normal shutdown. [6] Later that month, the TH-12 engine underwent a spot check hot fire test for the first flight batch, fully simulating the flight conditions of the inaugural Tianlong-3 launch. The test involved 6 consecutive ignitions of the engine without removal from the test stand, accumulating a total test duration exceeding 1,000 seconds, with the single engine operating time surpassing the planned flight duration by a factor of 6. [7]

References [ edit ]

  1. ^ "天火-12 - 天火系列??机 - 天兵科技" . www.spacepioneer.cc . Space Pioneer . Retrieved 25 November 2022 .
  2. ^ "天兵科技百??液?火箭??机半系??????成功" . www.jiuyoucapital.com.cn . Retrieved 25 November 2022 .
  3. ^ Brugge, Norbert. "SpacePioneer" . www.b14643.de . Retrieved 25 November 2022 .
  4. ^ Chang, He. "天兵科技 110 ?液?火箭??机全系????成功" . ithome . Retrieved 25 November 2022 .
  5. ^ Space Pioneer. "?烈?祝天兵科技百??液?火箭??机 首???全系??程?????成功" (in Chinese (China)). Archived from the original on 2024-03-11 . Retrieved 11 March 2024 .
  6. ^ "?烈?祝天兵科技天?三?批???机校准????成功" (in Chinese (China)). Archived from the original on 2024-03-11 . Retrieved 11 March 2024 .
  7. ^ "?烈?祝天兵科技天?三?首?批次??机抽?????成功" (in Chinese (China)). Archived from the original on 2024-03-11 . Retrieved 11 March 2024 .