And it went well, no major glitches with the rocket itself, a pitot probe cover got stuck on adjacent structure after removal from the mast,
but the multiple delays were for errant ships in range safety corridor, and weather restrictions for first article flight parameters.
Burn-out was at 2 minutes with a 4 segment ET SRB stack as stage #1 and reached 28+ miles at stage separation.
It is designed to actually fly with a 5 segment stack, so that would have burned another 30 seconds and most likely doubled the velocity and altitute.
sao123
Direct and side mount are 2 very different competing SDLV - shuttle derived launch vehicles. No part of direct assumes anything about the ET, as it will have to be compltely redesigned and built for a lot more structureal integrity, just as it would be if Aries V would come to pass.
Everything about DIRECT assumes taking over the ET Tank structure, and converting it into a fuel sucking toad.
The ET System Derivative is based on the tank stack-up supplying fuel to an RS-24 engine set,
the same Space Shuttle Main Engines, and lifted with the assisted boost from a pair of ET SRB Boosters.
Only the Orbiter itself is not present.
Side-Mount or Top Mount - it doesn't matter.
The ET Tanks have no structural provision to attach RS-24 to anything on the aft dome of the oxygen tank,
and a mod like that would take 3 years, with lead times, just to make parts to install.
Then you've got that little problem of having to re-start the ET Tank line itself, which would not yield it's first tank assembly
ready to attempt modification adaption for two or more years.
There really isn't a pile of ET Tanks to pick from, a minimal amount of spare parts that they can group to re-start with,
and NASA sure as hell isn't going to just give all the tools and equipment - the only manufacturing facility in the world
that is large enough to handle the size of the tanks,
and the only Vertical Gem-Cor Auto-Riveting machine in existance to Elon Musk for his amusement,
without a big payment for everything it takes to make them on the NASA Facility.
Otherwise, he would have to design everything from scratch - the tank
and the building to assemble it, produce engineering designs,
get parts into the pipeline - with 2 or more years of lead time, train mechanics, assemble those parts when they come in,
and prove that his modified assembly meets all the safety criteria for Man Rated Space Flight Systems.
Even concurrent development couldn't merge the first engine attach structure to the first in-process tank for at least two years,
then after structural completion you have to apply the Thermal Protective System (FOAM) and ultimately test fire the structure
with engines to prove the system will not collapse the aft structural mounts and dome.
So there is 4 years gone and you've still got a 35 old peice of technology clinging to it's heritage - that's not progress,
that concept was abandoned by NASA over 20 years ago - for a reason.
Neither of the Atlas V and Delta IV based systems are Man-Rated,
and they would have to be re-designed as well to bring them up to safety standards.
Each costs 350 Million a pop to fly now, so enhancing them would be 2 more years of design evaluation, structural mods,
and then building and flying the prototype, and each unit for flight would exceed 450 Million as a man rated system.
Either of them would just be a Stage 1 propulsion system - you still need at least a second stage rocket system,
and Centaur won't cut it.
Ares-1 when fully functional is projected to cost 100 Million per launch when ready for LEO manned flight.
Boeing is builllding the Ares-1 Stage 2 booster now, early, but underway.
The entire game is to fund the project - you can nickle and dime it to death, and over-run the costs,
or do it right - not cheap, but correctly.
These are
REAL rockets, not models and toys.