Hi, this is my first post here, and it seems like an excellent forum and font of knowledge! I have been following the Direct proposal as it has evolved over on Nasaspaceflight forums and have found that it is treated somewhat differently here.
Given that I merely a lay person with no particular connection with any aerospace company or agency, I was quite convinced that Direct 2.0 would be cheaper and faster to develop than Ares I & V, for the following (simplistic) reasons:
- No need to develop a 5-segment RSRM
- No need to alter facilities to support 10m tanking or greater roll-out mass of the Ares-V.
- Development and support of a single vehicle rather than two
- As a smaller vehicle, with greater commonality with STS, J232 ought to be cheaper than Ares-V, although less powerful.
In addition to these potential costs savings, I was swayed by the idea that a vehicle with greater commonality with STS could surely be produced sooner, and further that having J120 ready in the mid 2010s would place the VSE in a much stronger position to survive any future budget cuts- surely a prudent way to operate.
It would appear that NASA has found otherwise, and today I found a link on this forum to a release stating so. However I simply do not understand how, for example, the Jupiter core stage could cost any more to develop and build than an Ares-V core stage. I also noticed an error in that report in which the J120 was said to be too expensive because it had three RS68s and a J2X-powered upper stage; that, of course, is a description of the J232 configuration.
Thanks for any replies,
John







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