Not Tengyun Project, which is a project under CASIC. This paper was published by employee from CASC instead, so a parallel development.
Unfortunately no, I would have posted it yesterday if I had the paper.Thanks. Do you have access to the paper? I'd like a copy if possible.
Depends on what is Tengyun project's definition. The particular LATS is NOT orbital launcher, the 2nd stage does not reach orbital velocity but rather a glider. It is same in principle to DF-17 but with much longer range that its 1st stage will leave atmosphere. It is essentially the longer ranged boost-glide craft in the book "高速远程精确打击飞行器方案设计方法与应用"Illustrations from paper on a HTHL spaceplane/transport plane. Might this be about the Tengyun project? Does anyone have access to the paper to provide more context?
Some specs based on the illustrations:
- Re-usability: >100 times
- Payload capacity: >60 tons
- Reliability: <0.997 (target goal), 0.97 (achieved)
- Speed: ≥10,000km
- Cost per launch: ~5% of single-use rockets