Quote from: Jim on 09/29/2022 04:16 pmQuote from: RickA on 09/29/2022 06:38 amTHIS is a large part of why I left NSF many years ago and why I will probably do so again very shortly. Try to be helpful or get people to be balanced about their thinking and you will be roasted for it.The anti SLS is warranted. Anything else is better. It is the SpaceX only fanatical young males are the issue.I'm with Rick. 95% of the discussion on this thread has been to complain about cost, schedule and flight rate. While valid issues, it is a dispiriting drumbeat. I would much rather have discussions on technical and programmatic changes that could improve the SLS program. The latter discussion would educate and maybe lead to positive improvements. For example:* Design improvements to mitigate hydrogen leaks and improve sensor reliability* FTS design changes to increase the batter life or allow for charging after installation* Pad flow improvements to reduce roll-out times* Identify and resolve bottleneck issues to increase production rate of SLS so that you could have a higher flight rate.* Co-manifest options with Orion* Mobile launcher upgrades to improve serviceability, weight, and alignment issues* Refueling of the core hydrogen tank in LEO as a cryo depot or wet workshop, perhaps after BOLE is implemented that could get the core into a stable LEO orbit.* Recovery and reusability upgrades for SLS components* Material science discussion on alternatives to the foam insulation around the core tank.Those are just a few ideas, many more are out there.
Quote from: RickA on 09/29/2022 06:38 amTHIS is a large part of why I left NSF many years ago and why I will probably do so again very shortly. Try to be helpful or get people to be balanced about their thinking and you will be roasted for it.The anti SLS is warranted. Anything else is better. It is the SpaceX only fanatical young males are the issue.
THIS is a large part of why I left NSF many years ago and why I will probably do so again very shortly. Try to be helpful or get people to be balanced about their thinking and you will be roasted for it.
Compared to what? The other two PRIVATE space programs? Weren't those big rockets supposed to launch.....2 years ago? Lit 7 out of 33 engines and then had to swap them out! Whoohoo! Then there's the other one with, no engines? But hey nice launch towers/pads and great inflight abort test! We don't know much more because they're PRIVATE.
Wasn't SLS supposed to launch in 2016?
This excercise to fix SLS would have been completely unnecessary if NASA had not bowed to political pressure and had just come up with a clean slate design.
A private-sector super-heavy rocket is yet to be proven. SpaceX is making great strides and they seem to be on the right track. More power to them, I hope they are successful. But that is at Elon Musk's discretion, SH/SS could be canceled at any time. Blue Origin seems to be stuck in permanent engine development mode with BE4, and nothing concrete about New Armstrong at all for years. All they have at the moment is New Shepard doing vertical 100 km hops, nowhere near reaching orbital speeds. At least they are getting good practice in on launch, land, and recovery.Am I missing anybody? Any other entries in the fiercely competitive super-heavy market segment? The fact is that there is no commercial market demand for super-heavy launch at this time.
To be fair, was there ever a real option that NASA would be able to design a clean-slate option?
I'm with Rick. 95% of the discussion on this thread has been to complain about cost, schedule and flight rate. While valid issues, it is a dispiriting drumbeat.
I listed a series of metrics with which to evaluate ANY project.
So the SLS has many good things about it:1) It uses LOX/LH22) It uses SSMEs
3) It uses advanced aluminum alloys with the core tanks that are colored with orange foam.That 95% good stuff by weightSo when folks oppose it, they cannot point to specific thing they’d change.However the Orion payload is a very non-inspirational design. It doesn’t invoke anything about innovation. Just looks like a capsule from the 60’s. People were pretty negative when about it was launched on a Delta launch vehicle. So hypothetically, what if there was a Starship on top of SLS? I think folks would be more positive.Again hypothetically, what if Orion was on top of a Super Heavy Booster? 😱. That would likely be a pretty awful sight.
Daily cursed rockets #164:Orion and ICPS on SuperheavyRequested by @starsea099
[NET 2022] 130.0 mt Starship, everything will be recovered, refuelable in orbit: ~$ 50 million
BO seems to do a pretty good job of staying private. IMO that's because there are not a lot of interesting things happening.
So hypothetically, what if there was a Starship on top of SLS? I think folks would be more positive.
So if I had to give up something from ARTEMIS I, you could get me to budge with Orion. It hasn’t flown any astronauts yet. And the basic concept of Orion seems too cramped and limiting for traveling to the lunar surface.
Quote from: mandrewa on 09/30/2022 05:14 pm[NET 2022] 130.0 mt Starship, everything will be recovered, refuelable in orbit: ~$ 50 millionNET 2025, if at all, for all 4.
Quote from: laszlo on 10/01/2022 11:05 amQuote from: mandrewa on 09/30/2022 05:14 pm[NET 2022] 130.0 mt Starship, everything will be recovered, refuelable in orbit: ~$ 50 millionNET 2025, if at all, for all 4.Why do you think this? you may be right of course. IMO SLS/Orion is riskier. It must either fly in November or not fly for at least a year, based on rollout-rollback and SRB constraints. We've seen that it only takes one little thing going wrong to stop a launch, so the November launch is statistically risky. I hope it launches, but it might not. If it launches, I hope the mission succeeds, but it might not.IMO Starship is more likely to launch in November. I hope it does. It's first goal (reach space) is easier than Artemis I and I think it will succeed. Its more ambitious goals are much less likely to be achieved.Vulcan continues to slip at a rate of about one month per month. This does not converge, but surely things will eventually change?
Quote from: DanClemmensen on 10/01/2022 03:37 pmQuote from: laszlo on 10/01/2022 11:05 amQuote from: mandrewa on 09/30/2022 05:14 pm[NET 2022] 130.0 mt Starship, everything will be recovered, refuelable in orbit: ~$ 50 millionNET 2025, if at all, for all 4.Why do you think this? you may be right of course. IMO SLS/Orion is riskier. It must either fly in November or not fly for at least a year, based on rollout-rollback and SRB constraints. We've seen that it only takes one little thing going wrong to stop a launch, so the November launch is statistically risky. I hope it launches, but it might not. If it launches, I hope the mission succeeds, but it might not.IMO Starship is more likely to launch in November. I hope it does. It's first goal (reach space) is easier than Artemis I and I think it will succeed. Its more ambitious goals are much less likely to be achieved.Vulcan continues to slip at a rate of about one month per month. This does not converge, but surely things will eventually change?It's because of what's left to do to develop and demonstrate all 4 of the features in mandrew's table. SS may very well make an orbital flight next month, but it won't fully reusable, (if at all), in-space refueling is only a gleam in Musk's eye with no hardware support on any of the SS yet, payload numbers are purely aspirational and will change depending on all the other changes required and the launch cost is based on a stack of as-yet unproven assumptions. That's not a slam on anyone, just saying the mandrew's metrics need some tweaking.
... IMO SLS/Orion is riskier. It must either fly in November or not fly for at least a year, based on rollout-rollback and SRB constraints. ...