That's good to know, but personally I'm more interested in knowing the diameter and volume of the spacecraft's pressure vessel, and even more importantly, the habitable volume. I think the Apollo command module's habitable volume is around 6.9 m^3 while the number for Orion is about 8.9 m^3. Since the angular slopes of the Apollo and Orion blunt cone shapes differ substantially from those of PTK-NP and Mengzhou, it's difficult to estimate the habitable volume of the latter two crafts without official sources (the PTK-NP, though about 4.5 m in diameter versus Orion's 5 metre, is quoted as having ~ 11m^3 of habitable volume due to the angular slope and the height of the design, assuming they're actively pursuing the program) . Hopefully CMSA will discuss Mengzhou's dimensional info in greater detail; or perhaps they did this already and I just didn't notice it?
(Never mind, I just noticed Rathalos' estimate of 14.5 m^3 of pressure vessel volume. Still the habitable volume would be of interest.)
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