3 ms·
Ah ha! In the back of my mind I knew this wasn't entirely unprecedented, just couldn't remember where. The scheme, as described in more details by you, is a l
by hga 13y ago
Ah ha! In the back of my mind I knew this wasn't entirely unprecedented, just couldn't remember where.
The scheme, as described in more details by you, is a lot simpler, and less concerning than I was envisioning (figures, given this is Space X). There's no cross tanking, that is, feeding the tanks of the central core from the sides.
Hmmm, although as I remember, when they had to shut down one engine during an ascent, it shed debris because of the pressure imposed by the adjacent engines. But I note the Merlin 1D, while producing significantly more thrust at sea level (nearly 50%), can throttle between 70-100 percent. Obviously they've thought through these stresses, and of course there are structural implications in making them highly reusable, they're willing to trade off weight penalties for durability, and therefore likely strength.
Anyway, thanks for the details, and all the contributions you've made to this topic!
- InclinedPlane 13y agoThat's a good point about the engine problem after it was shut down. However, there are a few important issues that are relevant. On further investigation the engine damage was due to fuel leakage, it wouldn't necessarily be expected that a healthy engine would react the same way if shut down under the same conditions. Also, that failure occurred at Max-Q (maximum dynamic pressure), and normally it would be expected that the stage separation would occur under much, much less strenuous aerodynamic conditions (farther down range and higher altitude, much lower atmospheric pressure).