Badenov
SOC-13
If atmospheric braking is described, then I assume LBB2 also provides stats for heat shields?LBB2.81, p34:
I never said it was efficient, I said it was possible. Also I haven't run the numbers or seen your math for a 25-50km runway, so is that mathed out or speculative? My math: The space shuttle lands at 344-364kph. Presuming that's the slowest velocity at which it can remain airborne, the takeoff velocity should be the same. At 1G thrust, you reach 354 kph or 98.3 m/s at 9.83 seconds (using 10m/s^2 as 1G, which Traveller seems to accept as an approximation). That's a takeoff roll of less than 500m, so forget the 25km runway. So like you said, 1G is a gargantuan amount of thrust for a TL7 commercial vehicle - it's substantial for a jet fighter!. Commercial aircraft take off with a quarter of that, flying bricks and F-4s take off with 60% of that. Aerodynamic launch with a full 1G of thrust is going to zoom. You don't need much aerodynamic lift with that much thrust.In this context, 10mm of vector length equates to -0.1G of deceleration in the vector movement system of LBB2.
Runways so long ... the curvature of the planetary surface prevents seeing the "far end" of the runway from the launch point.
So ... we're talking like 25-50 km long runways, right?
Sounds legit ...![]()
If we're looking at how much power you need for a tailsitter, the space shuttle launch system, with boosters and the big rocket in the tailsitter configuration, they alltogether have a thrust-to-weight of about 1.5 to 1, so about 0.5 in excess of local gravity, and that's what you'd need with 0 aerodynamic advantage.


