Quote from: edzieba on 09/02/2022 12:57 pmThe bellows are an complete nonissue: the 'problem' of how to have flexible cryogenic couplings on a rigid but moveable linkage without those bellow being load-bearing is not only a solved problem, but there is a solution currently sat on top of the arm halfway up the orbital launch tower, with said solution having already demonstrated the capability to move around, connect to a ship, and transfer cryogenic propellants.The arm can handle a small amount of translation, from wind and thermal expansion. But the amount of torsion on orbit in an emergency is much, much larger. There's no way that the arm hardware could withstand that. QuoteQuote from: TheRadicalModerate on 09/01/2022 11:25 pm3) Dorsal-to-dorsal nose-to-tail, overlapped docking. This could be androgynous, but it can also have full plumbing coming out of one payload bay and a stub that just stabilizes things in the other. (I think I've given up on this one.)4) Dorsal-to-dorsal, noses in the same direction, but overlapped docking, with the payload bay of one close to the tail QD of the other. In this case, the single grapple and the plumbing are all that's taking the torsional loads.OTV Booster seems to be on Team #2. I think edzieba and I are mostly on Team #4 (although we disagree on whether the torsional loads are a problem). I used to like #3, but I think #4 does everything it does and is simpler, moments of inertia permitting.I'm in camp 3, because it means all your drain-propellant-in-orbit-for-transfer plumbing is at the apex of the tanks and out of the way during normal operations, rather than at the nadir where all the drain-propellant-for-propulsion plumbing also needs to be. It also minimises torque about the connection, and minimises the movement of the centre of mass of the system (think of the setup as a heavy glob of propellants that some rigid lightweight shells happen to move around the outside of). It also allows for a 'bumper' to be deployed at the 'unused' (or inactive) nose-to-tail meeting point to aid bracing, if needed.When I went and actually drew this out, I got horribly confused, but Option #2 starts to look a lot better. Take a look and see what you think. Option #3 is really complicated, although it does indeed separate the transfer sources from the engine sumps, and it's the most mechanically stable. Note that the pros and cons haven't been thought through completely, but are a nice basis for discussion (or the hurling of rotten fruit). ¯\_(ツ)_/¯
The bellows are an complete nonissue: the 'problem' of how to have flexible cryogenic couplings on a rigid but moveable linkage without those bellow being load-bearing is not only a solved problem, but there is a solution currently sat on top of the arm halfway up the orbital launch tower, with said solution having already demonstrated the capability to move around, connect to a ship, and transfer cryogenic propellants.
Quote from: TheRadicalModerate on 09/01/2022 11:25 pm3) Dorsal-to-dorsal nose-to-tail, overlapped docking. This could be androgynous, but it can also have full plumbing coming out of one payload bay and a stub that just stabilizes things in the other. (I think I've given up on this one.)4) Dorsal-to-dorsal, noses in the same direction, but overlapped docking, with the payload bay of one close to the tail QD of the other. In this case, the single grapple and the plumbing are all that's taking the torsional loads.OTV Booster seems to be on Team #2. I think edzieba and I are mostly on Team #4 (although we disagree on whether the torsional loads are a problem). I used to like #3, but I think #4 does everything it does and is simpler, moments of inertia permitting.I'm in camp 3, because it means all your drain-propellant-in-orbit-for-transfer plumbing is at the apex of the tanks and out of the way during normal operations, rather than at the nadir where all the drain-propellant-for-propulsion plumbing also needs to be. It also minimises torque about the connection, and minimises the movement of the centre of mass of the system (think of the setup as a heavy glob of propellants that some rigid lightweight shells happen to move around the outside of). It also allows for a 'bumper' to be deployed at the 'unused' (or inactive) nose-to-tail meeting point to aid bracing, if needed.
3) Dorsal-to-dorsal nose-to-tail, overlapped docking. This could be androgynous, but it can also have full plumbing coming out of one payload bay and a stub that just stabilizes things in the other. (I think I've given up on this one.)4) Dorsal-to-dorsal, noses in the same direction, but overlapped docking, with the payload bay of one close to the tail QD of the other. In this case, the single grapple and the plumbing are all that's taking the torsional loads.OTV Booster seems to be on Team #2. I think edzieba and I are mostly on Team #4 (although we disagree on whether the torsional loads are a problem). I used to like #3, but I think #4 does everything it does and is simpler, moments of inertia permitting.
When I went and actually drew this out, I got horribly confused, but Option #2 starts to look a lot better. Take a look and see what you think. Option #3 is really complicated, although it does indeed separate the transfer sources from the engine sumps, and it's the most mechanically stable. Note that the pros and cons haven't been thought through completely, but are a nice basis for discussion (or the hurling of rotten fruit). ¯\_(ツ)_/¯
Quote from: TheRadicalModerate on 09/02/2022 08:15 pmWhen I went and actually drew this out, I got horribly confused, but Option #2 starts to look a lot better. Take a look and see what you think. Option #3 is really complicated, although it does indeed separate the transfer sources from the engine sumps, and it's the most mechanically stable. Note that the pros and cons haven't been thought through completely, but are a nice basis for discussion (or the hurling of rotten fruit). ¯\_(ツ)_/¯The options are complex. A key question would be how much specific work needs to be done to get from a standard Starship to a tanker (or depot) variant?SX likes to avoid special versions of stuff as long as possible (F9 and cargo Dragon were flying looong before FH and crew Dragon started flying). Also once SS starts making orbit they will want it to start being productive. That means starlink launches. This suggests they would prefer options that either a)Can be installed (or removed) as a package or b) Can be permanently installed on all SS because the payload hit is minor or zero.
Quote from: TheRadicalModerate on 09/02/2022 08:15 pmThe options are complex. A key question would be how much specific work needs to be done to get from a standard Starship to a tanker (or depot) variant?SX likes to avoid special versions of stuff as long as possible (F9 and cargo Dragon were flying looong before FH and crew Dragon started flying). Also once SS starts making orbit they will want it to start being productive. That means starlink launches. This suggests they would prefer options that either a)Can be installed (or removed) as a package or b) Can be permanently installed on all SS because the payload hit is minor or zero.Sounds right to me. It also makes me lean more toward Option #2, where the existing plumbing is used, and there's an adapter to allow two female QDs to talk to a male-male adapter.I think you could make something like the attached deploy out of the payload bay. At an arm-wave, you have payload bay doors that open and slide out a stowed version of everything you need. Then the stowed version needs to unfold itself as it extends back along the dorsal surface. All mechanical engineering that I attempt always turns out to be a kludge, but I can draw a block diagram.If you do this right, this is a complete "depot kit" that can turn any lift tanker into a depot or, more accurately, a tanker that's enabled to manage the transfer of prop in either direction. The sole modification you need on vanilla Starships or lunar Starships to use this is a pair of passive posts for the grapples to grab. (Note that "active" and "passive" refer to Starships with and without depot kits. They don't denote the direction of fueling. Depots have to be able to both receive and send prop.)Ideally, a deployed depot kit could re-stow itself, allowing the tanker to which it was attached to return to EDL. If that could happen, then there's no need for depots in cislunar orbits, which are likely more varied than the LEO orbit(s) needed for refueling. A tanker with a stowed depot kit can refuel at the LEO depot, boost to whatever cislunar (or HEEO) orbit is required, deploy its depot kit, refuel whatever LSS or vanilla Starship needs it, stow the kit, and return directly to EDL, where it can be reused as an ordinary tanker.If the kit can't re-stow, then you have permanent depots in cislunar that can't return. In this case, you have a passive tanker (no depot kit) that refuels at the LEO depot, boosts to the cislunar orbit (or HEEO) in which a second depot lives, refuels it, and then returns to EDL. Not quite as good or as flexible, but almost.
The options are complex. A key question would be how much specific work needs to be done to get from a standard Starship to a tanker (or depot) variant?SX likes to avoid special versions of stuff as long as possible (F9 and cargo Dragon were flying looong before FH and crew Dragon started flying). Also once SS starts making orbit they will want it to start being productive. That means starlink launches. This suggests they would prefer options that either a)Can be installed (or removed) as a package or b) Can be permanently installed on all SS because the payload hit is minor or zero.
A "gender bender" is an adaptor that's male on one side and female on the other, with plumbing crossed over as needed to make it work. (Otherwise it'll be the mirror image of what you want on one side or the other.) Are we in agreement here?
[diagram has a part labeled "gender bender"]
Quote from: TheRadicalModerate on 09/02/2022 08:15 pm[diagram has a part labeled "gender bender"]Fortunately there's no need for this.
Quote from: Twark_Main on 09/04/2022 03:31 pmQuote from: TheRadicalModerate on 09/02/2022 08:15 pm[diagram has a part labeled "gender bender"]Fortunately there's no need for this.But there's probably a need for something, if only to create a ship-to-ship separation that's manageable. Also, whatever you wind up using still has to function as a genuine QD. I imagine that an androgynous topology (which I agree is easy) is a little bit dicier to engineer for a clean, reliable separation at liftoff. Not impossible, but if you need something anyway, why fool with best practice?
If going the depot approach, would the Super Heavy booster not be a good fit to serve as the tanker?
Quote from: wes_wilson on 09/04/2022 08:04 pmIf going the depot approach, would the Super Heavy booster not be a good fit to serve as the tanker?It's going to be a while before they need to accumulate more prop than will fit in one Starship. Hence, a Starship will make a perfectly acceptable depot.When they finally do get to the point where they need more prop than a single Starship will hold, a SuperHeavy would be a pretty terrible waste of perfectly good engines. Even if they need four or five Starship-sized depots for some massive mission, that's still fewer engines than a single SuperHeavy.Last but hardly least, turning a SuperHeavy into a depot is a lot of work. Getting Starship ready to be refueled is probably about 75% of the work you'd need to get a Starship-based depot up and running, but roughly 0% of the work you'd need to get an SH-based depot going.PS: Just noticed that you said SH as the tanker, not the depot. That won't work. If you get an SH into orbit, it's not coming down. The reason it can do RTLS is because it's not going that fast at separation. At reentry from orbital speed, it'll burn up.
Quote from: TheRadicalModerate on 09/04/2022 07:31 pmQuote from: Twark_Main on 09/04/2022 03:31 pmQuote from: TheRadicalModerate on 09/02/2022 08:15 pm[diagram has a part labeled "gender bender"]Fortunately there's no need for this.But there's probably a need for something, if only to create a ship-to-ship separation that's manageable. Also, whatever you wind up using still has to function as a genuine QD. I imagine that an androgynous topology (which I agree is easy) is a little bit dicier to engineer for a clean, reliable separation at liftoff. Not impossible, but if you need something anyway, why fool with best practice?This has probably been shot down somewhere in the prior 28 pages, but I couldn't find it skimming through. If going the depot approach, would the Super Heavy booster not be a good fit to serve as the depot tanker? Other threads have indicated it's ssto capable. It and starship already have ports used for fueling starship while they're both on the OLM. It and starship already have some clamping mechanisms that hold them together through stage separation. Put a sh in orbit, use it as the depot/accumulator. Filled, it would hold nearly 3 starships worth of fuel/oxidizer. Lastly, although it has no heatshield, it has enough dv to reach orbit. There, it can be refueled by starships and then it would have the same dv as when sitting on the ground. Which is enough dv to be brought back without a heatshield for occasional and infrequent on-ground servicing. Has there been an exploration of using SH as the depot? Seems a closer starting point than using Starship.
I imagine that an androgynous topology... is a little bit dicier to engineer for a clean, reliable separation at liftoff.
Androgynous means face to face seals along the lines of a Westinghouse air brake glad hand but cryo rated.
"Eta Space announces Cryo-Dock™, a full scale commercial propellant depot capable of refueling multiple spacecraft with cryogenic propellants. Cryo-Dock™ design is already underway and is aimed to launch after the LOXSAT-1 mission funded by NASA. Eta Space is focused on cryogenic fluid management (CFM) technologies for the New Space Age and Clean Energy Economy."
We are back full circle. Androgynous means face to face seals along the lines of a Westinghouse air brake glad hand but cryo rated.
The adapter you described is essentially the free flyer without free flying. A semi-rhetorical question: is it easier/lighter/cheaper to design/build a mechanism to move the adapter down the hull or to put a small cold gas RCS+translation system on the adapter? It's hard to judge with so many final details TBD, but the question will always be there.
This option, #2, seems far and away the most sensible except for the question of how the gender bender gets put in place. It can't be there at launch time or else it'd violate the no-protrusion rule, and if it's extruded after launch, I think that amounts to making a big change to the vehicle. (But maybe not--like I said; I'm no expert.) If it has to be moved into place, it either needs to fly there (which seems a lot of new hardware!) or else someone needs to put it there (which violates the all-automatic rule).
This option, #2, seems far and away the most sensible except for the question of how the gender bender gets put in place. It can't be there at launch time or else it'd violate the no-protrusion rule, and if it's extruded after launch, I think that amounts to making a big change to the vehicle.
I don't see how this option (#3) can work at all. Not only does it have lots of new plumbing, I don't see how it can do the ullage burn without spinning like a pinwheel or (maybe) having the acceleration at a crazy angle. (Maybe I just lack imagination.)
You've still got the problem of holding the two vehicles together during fueling. I don't have any ideas for how to make that work, short of hoping that synchronized flying isn't infeasible, given the very low accelerations involved.
This, but • Delete the gender-bender and implement androgynous mirror-symmetrical interface plate • Tilt the interface plates at a slight angle, so the Starships have clearance between them • For docking the Starships both rotate and translate into position. This is done so the (off-axis) docking kick will exactly null out the rotation+translation. You "just" time-reverse the kinematics to find the exact docking approach maneuver.
Quote from: TheRadicalModerate on 09/04/2022 07:31 pm I imagine that an androgynous topology... is a little bit dicier to engineer for a clean, reliable separation at liftoff.Why?