Earlier quoted context omitted.
Nope. > Read the IFT-3 pre-flight materials I did. > They clearly intended to enter an orbital trajectory and then get out of it Nope, they very clearly did not. Even the graphic you linked to earlier shows this very clearly. https://blogger.googleusercontent.com/img/b/R29vZ2xl/AVvXsEi... 1. At step 4 for Starship, they write "Once S28 has reached orbital velocity ..." Not trajectory . Not orbit . 2. At step 8, we ha…
Orbital velocity = orbital speed + orbital trajectory. Velocity is a vector. Orbital velocity + orbital altitude means orbit. That is, unless you think that everyone at SpaceX misspoke and they were only aiming for orbital speed (which they did not achieve with IFT3), and just wanted that speed in any direction. Sounds like the plan to de-orbit was then to just go belly forward and let drag take you out of orbit. Tha…
The trajectory was suborbital, the perigee was inside earth so the actual trajectory would intersect the earth's surface, and the atmosphere first.