This is a young company with a staff of fewer than 50 people. Join them.do you know anything about this company? I can't find their website in English or Chinese.
This is a young company with a staff of fewer than 50 people. Join them.do you know anything about this company? I can't find their website in English or Chinese.
Isn't the YF-100K already tested and in production on the LM-12?I think it's all the engines of the CZ-10 (YF-100K, M, YF-75E), the hypergol lunar crew spacecraft RCS engine and the LOX-Methane engine for SAST's 4m dia rocket.
An illustration of the astroid dust detector and analyzer to be carried by the Tianwen-2 astroid sample return mission.
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Just asking, do you guys have any idea when the old hypogolics rockets will be retired for the new cryogenic long march rockets that are now operational ?Isn't the YF-100K already tested and in production on the LM-12?
Not for a few more years. Certainly not until the CZ-2F/Shenzhou is retired.Just asking, do you guys have any idea when the old hypogolics rockets will be retired for the new cryogenic long march rockets that are now operational ?
I suppose the old long march hypogolics rockets are soon due for retirement this coming years?
They have been prioritising cost-efficient platforms, so not for another 5 years until the reusable rockets become fully operational.Just asking, do you guys have any idea when the old hypogolics rockets will be retired for the new cryogenic long march rockets that are now operational ?
I suppose the old long march hypogolics rockets are soon due for retirement this coming years?
The transporter erector launcher (TEL) for the Zhuque-3 rocket being tested with a simulated load.
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I think this rocket will be crucial for China. It will have so many different uses if successful. Good luck.Zhuque-3 is on track for maiden flight in the second half of this year. The launch vehicle is of stainless steel construction. It has a body diameter of 4.5 meters, a fairing diameter of 5.2 meters, a total length of 76.6 meters, a takeoff mass of 660 tons, and a LEO carrying capacity of 21.3 tons. The 1st stage is designed to be reused no less than 20 times.
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