Quote from: Greg Hullender on 03/16/2025 11:42 pmElon's Orbital Garage! "Best prices for Meth and Lox above the Karmen Line!"Next stop for methalox in 1.3 light minutes!
Elon's Orbital Garage! "Best prices for Meth and Lox above the Karmen Line!"
Yes, if you're sure an engine failure isn't going to blow up the depot you just spent ten launches to fill up. it may take quite a bit of experience with reuse before anyone is confident of that though.
Quote from: TheRadicalModerate on 03/18/2025 07:08 pmAnd depots are cheap. If they have even a 10-mission lifetime, that's going to be about $1.5M/mission in costs. How do you figure this? Estimates I find just searching the web suggest it would cost ~$30 million to build one plus (if it's full) the cost of all the launches to fill it up, say, another $100 million. So if you lose a full one, you're out $130 million plus whatever the cost of the delay getting another one up and fueled. That's assuming it doesn't require lots of custom stuff like extensive solar panels for active cooling.
And depots are cheap. If they have even a 10-mission lifetime, that's going to be about $1.5M/mission in costs.
All we're arguing about is how likely one less-recently maintained engine is going to be to generate a catastrophic failure over one that's more recently maintained. At that particular failure node, it's probably a non-trivial difference. But you're more interested in getting through the whole tree with no problems.
I will confess that part of my obsession with stationary depots is that I see them as the core of a useful space station, particularly if you can eliminate ullage burns. I'm visualizing a space drydock that can maintain vehicles that never EDL with two depots attached by cables (one up, one down) that are long enough for tidal forces to do the ullage settling. (250 m gets you 1 mm/sec). But that doesn't work if the depots need to fly off.
Even on Earth, nobody puts the mechanics' garage next to the gas pumps any more.
Quote from: TheRadicalModerate on 03/19/2025 07:04 pmEven on Earth, nobody puts the mechanics' garage next to the gas pumps any more.You've not visited a small town.
Quote from: Greg Hullender on 03/19/2025 01:34 pmI will confess that part of my obsession with stationary depots is that I see them as the core of a useful space station, particularly if you can eliminate ullage burns. I'm visualizing a space drydock that can maintain vehicles that never EDL with two depots attached by cables (one up, one down) that are long enough for tidal forces to do the ullage settling. (250 m gets you 1 mm/sec). But that doesn't work if the depots need to fly off.Even on Earth, nobody puts the mechanics' garage next to the gas pumps any more.
Low Earth Orbit.[...]Missions beyond LEO will also require a tanker version of Starship for propellant aggregation. During these missions, SpaceX will launch one or more propellant tanker versions of Starship. Some of these tanker variants will remain in LEO as “depots,” and will be filled with propellant by subsequent tanker launches. LEO operations will occur in a circular orbit at 281 km altitude (+/- 100 km) and an inclination ranging from equatorial (0 degrees) to polar.Medium-Earth Orbit/High-Earth Orbit/Final Tanking Orbit. Missions beyond LEO will also require space station operations in medium-Earth orbit (“MEO”) to high-Earth orbit (“HEO”). For example, crewed lunar missions will include a secondary propellant transfer in MEO/HEO, the Final Tanking Orbit (“FTO”). Operations in MEO/HEO will occur in an elliptical orbit of 281 km x 34,534 km and an altitude tolerance of +116,000/-24,000 km apogee and +/- 100 km perigee, with inclination between 28 and 33 degrees (+/- 2 degrees).
The Technical Annex in SAT-LOA-20241218-00288 discusses propellant transfer.QuoteLow Earth Orbit.[...]Missions beyond LEO will also require a tanker version of Starship for propellant aggregation. During these missions, SpaceX will launch one or more propellant tanker versions of Starship. Some of these tanker variants will remain in LEO as “depots,” and will be filled with propellant by subsequent tanker launches. LEO operations will occur in a circular orbit at 281 km altitude (+/- 100 km) and an inclination ranging from equatorial (0 degrees) to polar.Medium-Earth Orbit/High-Earth Orbit/Final Tanking Orbit. Missions beyond LEO will also require space station operations in medium-Earth orbit (“MEO”) to high-Earth orbit (“HEO”). For example, crewed lunar missions will include a secondary propellant transfer in MEO/HEO, the Final Tanking Orbit (“FTO”). Operations in MEO/HEO will occur in an elliptical orbit of 281 km x 34,534 km and an altitude tolerance of +116,000/-24,000 km apogee and +/- 100 km perigee, with inclination between 28 and 33 degrees (+/- 2 degrees).
Quote from: StraumliBlight on 03/31/2025 02:08 pmThe Technical Annex in SAT-LOA-20241218-00288 discusses propellant transfer.QuoteLow Earth Orbit.[...]Missions beyond LEO will also require a tanker version of Starship for propellant aggregation. During these missions, SpaceX will launch one or more propellant tanker versions of Starship. Some of these tanker variants will remain in LEO as “depots,” and will be filled with propellant by subsequent tanker launches. LEO operations will occur in a circular orbit at 281 km altitude (+/- 100 km) and an inclination ranging from equatorial (0 degrees) to polar.Medium-Earth Orbit/High-Earth Orbit/Final Tanking Orbit. Missions beyond LEO will also require space station operations in medium-Earth orbit (“MEO”) to high-Earth orbit (“HEO”). For example, crewed lunar missions will include a secondary propellant transfer in MEO/HEO, the Final Tanking Orbit (“FTO”). Operations in MEO/HEO will occur in an elliptical orbit of 281 km x 34,534 km and an altitude tolerance of +116,000/-24,000 km apogee and +/- 100 km perigee, with inclination between 28 and 33 degrees (+/- 2 degrees).This does seem to suggest that SpaceX still doesn't see depots being a separate build, or going beyond LEO. I think this pushes us towards there being some kind of "depot kit" as TRM mentioned upthread?
Quote from: TheRadicalModerate on 03/19/2025 07:04 pmQuote from: Greg Hullender on 03/19/2025 01:34 pmI will confess that part of my obsession with stationary depots is that I see them as the core of a useful space station, particularly if you can eliminate ullage burns. I'm visualizing a space drydock that can maintain vehicles that never EDL with two depots attached by cables (one up, one down) that are long enough for tidal forces to do the ullage settling. (250 m gets you 1 mm/sec). But that doesn't work if the depots need to fly off.Even on Earth, nobody puts the mechanics' garage next to the gas pumps any more.You've not visited a small town.
Quote from: TheRadicalModerate on 03/19/2025 07:04 pmQuote from: Greg Hullender on 03/19/2025 01:34 pmI will confess that part of my obsession with stationary depots is that I see them as the core of a useful space station, particularly if you can eliminate ullage burns. I'm visualizing a space drydock that can maintain vehicles that never EDL with two depots attached by cables (one up, one down) that are long enough for tidal forces to do the ullage settling. (250 m gets you 1 mm/sec). But that doesn't work if the depots need to fly off.Even on Earth, nobody puts the mechanics' garage next to the gas pumps any more.I was going to put them at least 250 m apart. :-) Even a couple of km of cable probably presents no problem, and it makes the problem a bit easier in cases where one depot is empty but the other is not.
If that was true, ISS wouldn’t exist. The debris issue is proportional to cross sectional area, not length.
Quote from: Greg Hullender on 03/20/2025 12:07 amQuote from: TheRadicalModerate on 03/19/2025 07:04 pmQuote from: Greg Hullender on 03/19/2025 01:34 pmI will confess that part of my obsession with stationary depots is that I see them as the core of a useful space station, particularly if you can eliminate ullage burns. I'm visualizing a space drydock that can maintain vehicles that never EDL with two depots attached by cables (one up, one down) that are long enough for tidal forces to do the ullage settling. (250 m gets you 1 mm/sec). But that doesn't work if the depots need to fly off.Even on Earth, nobody puts the mechanics' garage next to the gas pumps any more.I was going to put them at least 250 m apart. :-) Even a couple of km of cable probably presents no problem, and it makes the problem a bit easier in cases where one depot is empty but the other is not.A couple kilometers of cable isn't going to last long in LEO. MMOD isn't kind to long tethers.
In the three-cable arrangement, I wouldn't want to be nearby when one of those cables snaps. I definitely don't want to be in a fragile tin can that's holding my air in. The first rule of cable safety is that you don't stand directly in-line with the cable. The Shuttle tether experiment failed due to a broken cable, and this wasn't even caused by a MMOD strike.
Quote from: Twark_Main on 04/14/2025 02:05 amIn the three-cable arrangement, I wouldn't want to be nearby when one of those cables snaps. I definitely don't want to be in a fragile tin can that's holding my air in. The first rule of cable safety is that you don't stand directly in-line with the cable. The Shuttle tether experiment failed due to a broken cable, and this wasn't even caused by a MMOD strike.I think it'll need a mechanical engineer to offer a useful opinion here. It doesn't seem like a big deal to me, given the small forces involved, but an expert would know--and know how to mitigate risks like that.
Quote from: Greg Hullender on 04/14/2025 04:03 pmQuote from: Twark_Main on 04/14/2025 02:05 amIn the three-cable arrangement, I wouldn't want to be nearby when one of those cables snaps. I definitely don't want to be in a fragile tin can that's holding my air in. The first rule of cable safety is that you don't stand directly in-line with the cable. The Shuttle tether experiment failed due to a broken cable, and this wasn't even caused by a MMOD strike.I think it'll need a mechanical engineer to offer a useful opinion here. It doesn't seem like a big deal to me, given the small forces involved, but an expert would know--and know how to mitigate risks like that.Cable snap-back isn't exactly a controversial hazard when it comes to lines under tension.The mitigation is to not let the cable snap. To reduce damage you can reduce the strain energy, but ultimately you're limited by the cable material. A thin pressurized steel tank covered by a lightweight whipple shield isn't going to stand up well.I hope you can let us know what your mechanical engineer friend says. I'll be very interested to hear it!