This is true. The engines overperformed and they're going a lot further than they meant to. This is better than anticipated news.
It's only bad if you're REALLY focused on the Tesla "going to Mars", which it was never really going to do, because it would need to slow down once it got to Mars to stay in orbit around it. What we've done is prove capability. Getting to Mars is 100% possible, and we've also proven fault tolerance ... that is, we have enough fuel to spare that we can make correction-burns if necessary during the trip to Mars.
> that is, we have enough fuel to spare that we can make correction-burns if necessary during the trip to Mars.
Stage 2 of the Falcon would not be used for long flights. This was the longest it ever coasted (6 hours). Any longer, and you run into all sorts of limitations: running out of batteries, RP-1 freezing, and LOX boiling off.
For longer trips, stage 2 would separate after the earth escape burn and the craft's own propulsion system would take over.
I was thinking of right transfer orbit combined with exactly right aerobraking, though I'm not sure if Mars has a dense enough atmosphere even if you were aiming for a flyby 1 millimeter above the surface (and that's assuming an indestructible Roadster)...
You need a third body to pull that off, and I think Mars’s moons are too small to be useful for this.
Looking at practical considerations rather than just theoretical, you also need the ability to perform course corrections along the way. The initial trajectory won’t be precise enough to make it work from just the departure burn.
Yep. Real-Scale Solar System provides that. There are also mods to add real-world rockets (like the Falcon Heavy) and real-world aerodynamics (Ferram Aerospace Research).
To do a gravity assist you do not need anything more than Newtonian two-body interaction. KSP already has that.
You can think of it as a small ball (the vehicle) bouncing of a big heavy ball (the planet), but the forces are not those of elastic compression, rather those of gravity.
You're agreeing with his point. The plan was not to orbit Mars.
However, your language sounds like they were going to circularize at 'about the distance of mars', which they were not (that too would have required a burn months from now). The plan they'd previously briefed was an elliptical orbit where the aphelion is ~Mars' orbitial distance (~1.5AU) and the perihelion is still at Earth's orbital distance (~1AU). However, with the extended burn, they got the aphelion up to 2.61 AU.
It's only bad if you're REALLY focused on the Tesla "going to Mars", which it was never really going to do, because it would need to slow down once it got to Mars to stay in orbit around it. What we've done is prove capability. Getting to Mars is 100% possible, and we've also proven fault tolerance ... that is, we have enough fuel to spare that we can make correction-burns if necessary during the trip to Mars.