Has anybody any information concerning possible alternative uses for the Space Shuttle's External Tank? I know that there were some plans to use it as part of a space station project, but were there any other proposed uses for them?
blackstar said:Really amazingly detached from reality. [...] Or maybe they have the video on their website.
FutureSpaceTourist said:
- "we will create a fleet of dramatically improved, safer and lower cost shuttles"
Nik said:IIRC, there were still-born plans for Shuttles to 'burn the tank dry' and carry it into orbit.
Sundry snags included the weight overheads, the severe restrictions on payloads --Flown Shuttles ran rather heavier than hoped-- and that pesky, crumbly foam. Then they'd need multiple space-walks to clad the exterior in reflective 'bumper' layers which would have to be hauled to orbit. Then there was the weight of space-rated hatches and connecting tunnels, which would have to be hauled to orbit and retrofitted due to their materials' incompatibility with cryo-stuff...
Oh, and the tankage was full of baffles which would need to be removed without leaving sharps...
blackstar said:But even a moderate amount of popcorning would leave your space station surrounded by a foam debris cloud.
Nik said:Only they didn't happen, either...
Nik said:IIRC, there were still-born plans for Shuttles to 'burn the tank dry' and carry it into orbit.
Sundry snags included the weight overheads, the severe restrictions on payloads --Flown Shuttles ran rather heavier than hoped-- and that pesky, crumbly foam. Then they'd need multiple space-walks to clad the exterior in reflective 'bumper' layers which would have to be hauled to orbit. Then there was the weight of space-rated hatches and connecting tunnels, which would have to be hauled to orbit and retrofitted due to their materials' incompatibility with cryo-stuff...
Oh, and the tankage was full of baffles which would need to be removed without leaving sharps...
Nik said:Given the way the Apollo / Saturn systems were not 'derived' for heavy lifts...
DaveJ576 said:Which brings up a good question concerning the viability of the AAP "Wet Workshop" approach. How much of a problem would it have truly been to outfit a S-IVB interior? Would this really have worked or not?
Michel Van said:i found a paper about a ET Space station
"Space Shuttle External Tank Used as a Space Station Study Project Perun"
online on Wikisource
http://en.wikisource.org/wiki/Perun_1979
There have been a bunch over the years. You should look up Space Island One for one of the crazier proposals (hint: they wanted to build an international fleet of 10 space shuttles).
One of the big problems with using the ET as a space station was that the foam shed in orbit, so you would have a lot of debris around the space station. Another problem is that structure is cheap, but all the stuff you put inside it is expensive, so an ET doesn't get you very much savings, just a lot of volume to fill up.
There were some more sane ideas, such as attaching a cargo pod at the rear of the ET and using the ET primarily as a strongback.
There is no "imagining", it needs to be based on facts and data and not day dreams. Explain yourself. External Tank has a large beam in it.Yet such an inert External Tank/SLS core would still be less a threat to LEO than the Starship I imagine…
no. The concept is not the issue. It is your statement "an inert External Tank/SLS core would still be less a threat to LEO than the Starship I imagine", this claim needs data to back it up.Mark Holderman did work on the GEODE concept...I don't think he is a "daydreamer" and knows all the specs--ask him.
Video:Hazegrayart said:Humpback Shuttle, External Tank Space Station
An undefined need for more payload bay volume inspired the thought that the lee side area above the payload bay (at entry angles of attack) could be used for an expanded bay. This resulted in what was called the “humpback” orbiter. The wind shield area was
faired into the higher moldline and whole faired into the vertical fin trailing edge. There was no change in the hypersonic aerodynamic characteristics at high angles of attack. However, there was no evaluation of the subsonic aerodynamic characteristics, but it is likely that there some degradation of directional stability.
STS External Tank Station
In 1980, NASA conducted a study on various concepts for an American manned space station, focusing on the 'wet workshop' approach. This concept involved using the large External Tank carried into orbit by each shuttle flight to create a spacious space station.
Although the idea was highly cost-effective and practical, NASA management ultimately did not pursue it seriously. The proposal was viewed as a tempting low-cost alternative to their own ambitious plans for a large modular space station.
https://youtu.be/0w4B0C_nBPg?si=CTVcMHCrBIpn4Vc8